189 20 8242 https://digitalprojects.uah.edu/files/original/109/7175/r01c09-35.pdf f5eb78473f748e61ac79fd37d6a825bd Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context Series 01, Subseries C: Cabaniss Personal Correspondence Title A name given to the resource Series 01, Subseries C: Cabaniss Personal Correspondence Description An account of the resource Subseries C, Cabaniss Personal Correspondence (CPC), consists of correspondence from letters from friends, relatives, and their children. Most of the family correspondence involves these children and families of S. D. Cabaniss, and his brothers and sisters who appeared to have been enormous burdens in these difficult years. These papers are sorted "to whom," "from whom," and then chronologically. Still Image A static visual representation. Examples include paintings, drawings, graphic designs, plans and maps. Recommended best practice is to assign the type Text to images of textual materials. Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context r01c09-35 Title A name given to the resource Fearn, Walker, and White Funeral/Death Notices Relation A related resource r01c-210910 Source A related resource from which the described resource is derived Frances C. Roberts Collection, Series 1, Subseries C, Box 9, Folder 35, University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama https://digitalprojects.uah.edu/files/original/131/9332/r09_01-06.pdf b502ec275e2d8d3f891529fef851469b Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context Series 09: Fearn, Donegan & Co. (F&D) Title A name given to the resource Series 09: Fearn, Donegan & Co. (F&D) Description An account of the resource These papers are a comprehensive set of Huntsville business papers of Dr. Thomas Fearn and James J. Donegan during their years (1837-1854) as cotton commissioners (cotton factors). The office in New Orleans particularly kept a steady business correspondence between the two offices. Included are papers one might expect to maintain a business at the times.<br />Included in Box 1 is a copy of a paper delivered by Dr. Roberts to the Alabama Historical Association in 1974, "Fearn, Donegan and Company: A Case Study of the Cotton Factorage System in the Tennessee Valley." Original partners of the company included Thomas Lockhart, Dr. Thomas Fearn, and James J. Donegan. Later Isaac W. Moon and Albert Crenshaw of New Orleans were partners, and then William P. Atwood. Matthew W. Steele and Arthur Mosley Hopkins of Huntsville joined the company, and still later Donegan's son, James H. Donegan after his graduation from Georgetown College worked for them.<br />These papers are sorted by year and then grouped as accounts, receipts, and statements; bills of lading receipts; correspondence from Liverpool, England, the New York office and balance sheets; business correspondence with local customers, then sorted generally by area; some few personally related correspondence (e.g. Weakley, Fearn, Donegan) court case; and a few telegrams. Still Image A static visual representation. Examples include paintings, drawings, graphic designs, plans and maps. Recommended best practice is to assign the type Text to images of textual materials. Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context r09_01-06 Source A related resource from which the described resource is derived Series 9, Box 1, Folder 6 Title A name given to the resource Fearn, Wilcox Checks, 1834 Relation A related resource r09-211014 https://digitalprojects.uah.edu/files/original/132/9366/r10_03-11.pdf 31572495eb02b239d0a65e1ad1aff68b Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context Series 10: Books and Pamphlets Title A name given to the resource Series 10: Books and Pamphlets Still Image A static visual representation. Examples include paintings, drawings, graphic designs, plans and maps. Recommended best practice is to assign the type Text to images of textual materials. Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context r10_03-11 Source A related resource from which the described resource is derived Series 10, Box 3, Folder 11 Title A name given to the resource Fearns of Virginia Description An account of the resource RESTRICTED. This book has been moved to a bookcase. Contact Archives staff for more information. Relation A related resource r10-211020 https://digitalprojects.uah.edu/files/original/204/14962/20250313_154612.jpg 7e4f53c3cc710cf611df80a07fa8911d Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context HON 399 Research in London Title A name given to the resource HON 399 Research in London Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Title A name given to the resource Feather-leaved banksia plant bed at Kew gardens. Creator An entity primarily responsible for making the resource Rasmussen, Kaleb Description An account of the resource A photo of Banksia Brownii (the feather-leaved banksia), a plant indigenous to the far south-western corner of Western Australia. It is currently listed as critically endangered with an estimate of only 1,000 plants in the wild. Date A point or period of time associated with an event in the lifecycle of the resource 2025-03-13 Source A related resource from which the described resource is derived Kaleb Rasmussen, HON 399-H01, Spring 2025. Language A language of the resource en Rights Information about rights held in and over the resource This material may be protected under U. S. Copyright Law (Title 17, U.S. Code) which governs the making of photocopies or reproductions of copyrighted materials. You may use the digitized material for private study, scholarship, or research. Though the University of Alabama in Huntsville Archives and Special Collections has physical ownership of the material in its collections, in some cases we may not own the copyright to the material. It is the patron's obligation to determine and satisfy copyright restrictions when publishing or otherwise distributing materials found in our collections. https://digitalprojects.uah.edu/files/original/108/6791/r01b25-00-025.pdf d1e639229ba48d03e9859011b82309b0 Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context Series 01, Subseries B: Cabaniss Professional Business Title A name given to the resource Series 01, Subseries B: Cabaniss Professional Business Description An account of the resource Sub series B (CPB) deals with a small, but active, legal practice of Septimus Cabaniss with his various partners, who included men considered to be outstanding lawyers in the state, from the 1890s to 1938 at the office on the town Square. He studied law in Huntsville under Silas Parsons and practiced law with Leroy Pope Walker, Robert C. Brickell, and Francis P. Ward. These papers are sorted by year, except when an obvious grouping of an estate is evident. The papers continue through professional activities at the Madison County Courthouse including those of his son, James Budd Cabaniss, and his daughter, Fanny Cabaniss, who were clerks of the Chancery Court and a few papers of his son, Septimus, Jr., who owned a bookstore for a brief period. Still Image A static visual representation. Examples include paintings, drawings, graphic designs, plans and maps. Recommended best practice is to assign the type Text to images of textual materials. Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context r01b25-00-025 Title A name given to the resource Federal Internal Revenue Laws, 1917 Relation A related resource r01b-210907 Source A related resource from which the described resource is derived Frances C. Roberts Collection, Series 1, Subseries B, Box 25, Item 25, University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama https://digitalprojects.uah.edu/files/original/104/5091/img_00503.pdf f02e66d86e631fc14a863e3e6a816456 Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Title A name given to the resource Southpaw Postcard Collection Identifier An unambiguous reference to the resource within a given context Southpaw Postcard Collection Description An account of the resource George (Buzz) & Peg Heeschen have allowed us to include their collection of about 500 Huntsville and Madison County postcards, including scenes of buildings, streets, homes, Big Spring, Monte Sano, Marshall Space Flight Center and many others. Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context img_00503;img_00504 Title A name given to the resource Federal Square Coverage The spatial or temporal topic of the resource, the spatial applicability of the resource, or the jurisdiction under which the resource is relevant 206 Greene Street SE Description An account of the resource Front: Federal Square, Huntsville, Ala. Type The nature or genre of the resource Postcards Subject The topic of the resource Public buildings (Huntsville, Ala.) Central business districts (Huntsville, Ala.) Huntsville (Ala.) Madison County (Ala.) Publisher An entity responsible for making the resource available C. T. American Art Colored Source A related resource from which the described resource is derived From the postcard collection of George and Peg Heeschen, The Southpaw, Huntsville, Alabama Provenance A statement of any changes in ownership and custody of the resource since its creation that are significant for its authenticity, integrity, and interpretation. The statement may include a description of any changes successive custodians made to the resource. This collection is digital only. Rights Information about rights held in and over the resource This material may be protected under U. S. Copyright Law (Title 17, U.S. Code) which governs the making of photocopies or reproductions of copyrighted materials. You may use the digitized material for private study, scholarship, or research. Though the University of Alabama in Huntsville Archives and Special Collections may have physical ownership of the material in its collections, in some cases we may not own the copyright to the material. It is the patron's obligation to determine and satisfy copyright restrictions when publishing or otherwise distributing materials found in our collections. Relation A related resource postcard_import-210603 Language A language of the resource en Spatial Coverage Spatial characteristics of the resource. 34.730992,-86.583767 https://digitalprojects.uah.edu/files/original/33/4722/loc_gold_000354_000354.pdf 88228e48b9bb3933d84751c7cdd1e1bd Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Title A name given to the resource Goldsmith-Schiffman Collection Identifier An unambiguous reference to the resource within a given context Goldsmith-Schiffman Collection Description An account of the resource <p>"My ancestors were all German Jewish immigrants, members of four families who settled in Huntsville, Alabama before and following the Civil War. The Bernstein, Herstein and Schiffman families arrived during the 1850s, and Oscar Goldsmith arrived in 1879. Subsequent generations united these four families in marriage. Members of the extended family have figured in every phase of the history of Huntsville, both economically and socially; from the agrarian years of the nineteenth century through Huntsville’s growth after World War II, to becoming known as Rocket City USA; and socially, from the time of institutionalized slavery before the Civil War to segregation followed by the civil rights era."</p> <p>-<a href="https://www.myjewishlearning.com/southern-and-jewish/highlighting-the-history-of-huntsvilles-jewish-community/">Margaret Anne Goldsmith in an interview with My Jewish Learning</a></p> Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context loc_gold_000354_000354 Title A name given to the resource Fee report for a claim suit filed by Lawrence Goldsmith against H. Oliver with Parks & Cotton. Description An account of the resource This document contains a detailed breakdown of the fees associated with the "unlawful detainer suit" filed by Lawrence Goldsmith against H. Oliver. Creator An entity primarily responsible for making the resource Griffin, Malvern U. Date A point or period of time associated with an event in the lifecycle of the resource 1917-01-04 Temporal Coverage Temporal characteristics of the resource. 1910-1919 Subject The topic of the resource Attorney and client Lawyers--Fees Huntsville (Ala.) Madison County (Ala.) Scottsboro (Ala.) Jackson County (Ala.) Type The nature or genre of the resource Correspondence Text Source A related resource from which the described resource is derived I. Schiffman and Company Box 99, Folder Misc. Correspondence University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama Language A language of the resource en Rights Information about rights held in and over the resource This material may be protected under U. S. Copyright Law (Title 17, U.S. Code) which governs the making of photocopies or reproductions of copyrighted materials. You may use the digitized material for private study, scholarship, or research. Though the University of Alabama in Huntsville Archives and Special Collections has physical ownership of the material in its collections, in some cases we may not own the copyright to the material. It is the patron's obligation to determine and satisfy copyright restrictions when publishing or otherwise distributing materials found in our collections. Relation A related resource loc_gold_2021_02 https://digitalprojects.uah.edu/files/original/109/7545/r01c01-29.pdf 9e091963be2b1644fd958f0dec60704d Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context Series 01, Subseries C: Cabaniss Personal Correspondence Title A name given to the resource Series 01, Subseries C: Cabaniss Personal Correspondence Description An account of the resource Subseries C, Cabaniss Personal Correspondence (CPC), consists of correspondence from letters from friends, relatives, and their children. Most of the family correspondence involves these children and families of S. D. Cabaniss, and his brothers and sisters who appeared to have been enormous burdens in these difficult years. These papers are sorted "to whom," "from whom," and then chronologically. Still Image A static visual representation. Examples include paintings, drawings, graphic designs, plans and maps. Recommended best practice is to assign the type Text to images of textual materials. Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context r01c01-29 Title A name given to the resource Fennel, S. P. to Cabaniss, Charles Eugene Relation A related resource r01c-210910 Creator An entity primarily responsible for making the resource Fennel, S.P. Subject The topic of the resource Thank-you notes Books Loans Male friendship Success Type The nature or genre of the resource Correspondence Language A language of the resource en Rights Information about rights held in and over the resource This material may be protected under U. S. Copyright Law (Title 17, U.S. Code) which governs the making of photocopies or reproductions of copyrighted materials. You may use the digitized material for private study, scholarship, or research. Though the University of Alabama in Huntsville Archives and Special Collections has physical ownership of the material in its collections, in some cases we may not own the copyright to the material. It is the patron's obligation to determine and satisfy copyright restrictions when publishing or otherwise distributing materials found in our collections. Source A related resource from which the described resource is derived Frances C. Roberts Collection, Series 1, Subseries C, Box 1, Folder 29, University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama https://digitalprojects.uah.edu/files/original/73/1521/spc_youn_000020_01.mp3 79940ad9dd2e9d29835dca478a564280 https://digitalprojects.uah.edu/files/original/73/1521/spc_youn_000020_02.mp3 b0d89be489b9a8fff641014c7cd6fb09 Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context Anthony Young Collection Title A name given to the resource Anthony Young Collection Relation A related resource <a href="http://libarchstor.uah.edu:8081/repositories/2/resources/1" target="_blank" rel="noreferrer noopener">View the Anthony Young Collection finding aid in ArchivesSpace</a> Description An account of the resource Anthony Young was born in 1950. He graduated from Pratt Institute with a B.A. degree in Industrial Design. Mr. Young has worked for over twenty years in the aerospace industries. He is an author, a scientist, and aerospace historian. Oral History A resource containing historical information obtained in interviews with persons having firsthand knowledge. Duration Length of time involved (seconds, minutes, hours, days, class periods, etc.) 0:53:59 Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context spc_youn_000020_01 spc_youn_000020_02 MC_8_020 Title A name given to the resource Ferenc Pavlics. Creator An entity primarily responsible for making the resource Young, Anthony Date A point or period of time associated with an event in the lifecycle of the resource 2005-08-30 Temporal Coverage Temporal characteristics of the resource. 2000-2009 Format The file format, physical medium, or dimensions of the resource Audiocassettes Type The nature or genre of the resource Interviews Audio Source A related resource from which the described resource is derived Young Collection University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama Language A language of the resource en Rights Information about rights held in and over the resource This material may be protected under U. S. Copyright Law (Title 17, U.S. Code) which governs the making of photocopies or reproductions of copyrighted materials. You may use the digitized material for private study, scholarship, or research. Though the University of Alabama in Huntsville Archives and Special Collections has physical ownership of the material in its collections, in some cases we may not own the copyright to the material. It is the patron's obligation to determine and satisfy copyright restrictions when publishing or otherwise distributing materials found in our collections. Relation A related resource clir_grant_audio_metadata Oral History https://digitalprojects.uah.edu/files/original/40/650/uah_uahp_0000097_web.pdf 46a30637adfa867d779360c095c84d77 PDF Text Text � Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Title A name given to the resource UAH Photograph Collection Identifier An unambiguous reference to the resource within a given context UAH Photograph Collection Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context uah_uahp_0000097 Title A name given to the resource Festivities at 1993 Fall-Der-All. Creator An entity primarily responsible for making the resource University of Alabama in Huntsville Date A point or period of time associated with an event in the lifecycle of the resource 1993 Temporal Coverage Temporal characteristics of the resource. 1990-1999 Subject The topic of the resource College students Student activities University of Alabama in Huntsville Huntsville (Ala.) Madison County (Ala.) Type The nature or genre of the resource Photographs Still Image Language A language of the resource en Rights Information about rights held in and over the resource This material may be protected under U. S. Copyright Law (Title 17, U.S. Code) which governs the making of photocopies or reproductions of copyrighted materials. You may use the digitized material for private study, scholarship, or research. Though the University of Alabama in Huntsville Archives and Special Collections has physical ownership of the material in its collections, in some cases we may not own the copyright to the material. It is the patron's obligation to determine and satisfy copyright restrictions when publishing or otherwise distributing materials found in our collections. Relation A related resource uah_uahp_2019_04 Source A related resource from which the described resource is derived UAH Photograph Collection University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama https://digitalprojects.uah.edu/files/original/133/9414/r11_02-00-001.pdf e6cbf79e141ae826f5411ed16b312727 Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context Series 11: Archivist File of Additional Material Title A name given to the resource Series 11: Archivist File of Additional Material Still Image A static visual representation. Examples include paintings, drawings, graphic designs, plans and maps. Recommended best practice is to assign the type Text to images of textual materials. Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context r11_02-00-001 Source A related resource from which the described resource is derived Series 11, Box 2, Item 1 Title A name given to the resource Field Glasses Belonging To: Sargeant Major Baker Roberts, 5th Battalion, Alabama Volunteer Infantry Relation A related resource r11-211020 https://digitalprojects.uah.edu/files/original/104/5177/img_00713.pdf 992801b3eb82f1213b54c0a1e48cb072 Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Title A name given to the resource Southpaw Postcard Collection Identifier An unambiguous reference to the resource within a given context Southpaw Postcard Collection Description An account of the resource George (Buzz) & Peg Heeschen have allowed us to include their collection of about 500 Huntsville and Madison County postcards, including scenes of buildings, streets, homes, Big Spring, Monte Sano, Marshall Space Flight Center and many others. Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context img_00713;img_00714 Title A name given to the resource Fields of Water Cress Description An account of the resource Front: Fields of Water Cress, Huntsville, Alabama, "Water Cress Capitol of the World"<br />Back: FIELDS OF WATER CRESS, HUNTSVILLE, ALA. "Water Cress Capitol of the World." This view repeated many times in Madison County - a county of many fine springs of clear, cool water necessary in growing the best water cress. Type The nature or genre of the resource Postcards Subject The topic of the resource Agriculture (Huntsville, Ala.) Huntsville (Ala.) Madison County (Ala.) Publisher An entity responsible for making the resource available Anderson News Company, Florence, Ala.<br />Photo by Bryson Studio, Huntsville<br />Curteichcolor Source A related resource from which the described resource is derived From the postcard collection of George and Peg Heeschen, The Southpaw, Huntsville, Alabama Provenance A statement of any changes in ownership and custody of the resource since its creation that are significant for its authenticity, integrity, and interpretation. The statement may include a description of any changes successive custodians made to the resource. This collection is digital only. Rights Information about rights held in and over the resource This material may be protected under U. S. Copyright Law (Title 17, U.S. Code) which governs the making of photocopies or reproductions of copyrighted materials. You may use the digitized material for private study, scholarship, or research. Though the University of Alabama in Huntsville Archives and Special Collections may have physical ownership of the material in its collections, in some cases we may not own the copyright to the material. It is the patron's obligation to determine and satisfy copyright restrictions when publishing or otherwise distributing materials found in our collections. Relation A related resource postcard_import-210603 Language A language of the resource en https://digitalprojects.uah.edu/files/original/104/5319/img_01065.pdf 583fa1a4c2c20c3f646d2f2fe2dcef5b Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Title A name given to the resource Southpaw Postcard Collection Identifier An unambiguous reference to the resource within a given context Southpaw Postcard Collection Description An account of the resource George (Buzz) & Peg Heeschen have allowed us to include their collection of about 500 Huntsville and Madison County postcards, including scenes of buildings, streets, homes, Big Spring, Monte Sano, Marshall Space Flight Center and many others. Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context img_01065;img_01066 Title A name given to the resource Fifth Saturn I Launch at Cape Kennedy Coverage The spatial or temporal topic of the resource, the spatial applicability of the resource, or the jurisdiction under which the resource is relevant Kennedy Space Center Description An account of the resource Back: The fifth Saturn I launch vehicle (SA-5) leaves the launch pad at Cape Kennedy, Fla., on Jan. 29, 1964. Nose cone painted black for special thermal experiment. Type The nature or genre of the resource Postcards Subject The topic of the resource George C. Marshall Space Flight Center (Huntsville, Ala.) Huntsville (Ala.) Madison County (Ala.) Publisher An entity responsible for making the resource available Scenic South Card Co., Bessemer, Ala. <br />Color by NASA Source A related resource from which the described resource is derived From the postcard collection of George and Peg Heeschen, The Southpaw, Huntsville, Alabama Provenance A statement of any changes in ownership and custody of the resource since its creation that are significant for its authenticity, integrity, and interpretation. The statement may include a description of any changes successive custodians made to the resource. This collection is digital only. Rights Information about rights held in and over the resource This material may be protected under U. S. Copyright Law (Title 17, U.S. Code) which governs the making of photocopies or reproductions of copyrighted materials. You may use the digitized material for private study, scholarship, or research. Though the University of Alabama in Huntsville Archives and Special Collections may have physical ownership of the material in its collections, in some cases we may not own the copyright to the material. It is the patron's obligation to determine and satisfy copyright restrictions when publishing or otherwise distributing materials found in our collections. Relation A related resource postcard_import-210603 Language A language of the resource en Date A point or period of time associated with an event in the lifecycle of the resource 1964 Temporal Coverage Temporal characteristics of the resource. 1960-1969 https://digitalprojects.uah.edu/files/original/20/10294/uprsatIBquafilrepandrelmatfilsciforsatquafilrepno13_071007102648.pdf 6f707cdc278336ba3e8c80233e59043b Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Title A name given to the resource Saturn V Collection Relation A related resource <a href="http://libarchstor.uah.edu:8081/repositories/2/resources/60" target="_blank" rel="noreferrer noopener">View the Saturn V Collection finding aid in ArchivesSpace</a> Identifier An unambiguous reference to the resource within a given context Saturn V Collection Description An account of the resource <p>The Saturn V was a three-stage launch vehicle and the rocket that put man on the moon. (Detailed information about the Saturn V's three stages may be found<span> </span><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_first_stage.html">here,<span> </span></a><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_second_stage.html">here,<span> </span></a>and<span> </span><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_third_stage.html">here.</a>) Wernher von Braun led the Saturn V team, serving as chief architect for the rocket.</p> <p>Perhaps the Saturn V’s greatest claim to fame is the Apollo Program, specifically Apollo 11. Several manned and unmanned missions that tested the rocket preceded the Apollo 11 launch. Apollo 11 was the United States’ ultimate victory in the space race with the Soviet Union; the spacecraft successfully landed on the moon, and its crew members were the first men in history to set foot on Earth’s rocky satellite.</p> <p>A Saturn V rocket also put Skylab into orbit in 1973. A total of 15 Saturn Vs were built, but only 13 of those were used.</p> Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context uprsatIBquafilrepandrelmatfilsciforsatquafilrepno13_071007102648.pdf spc_stnv_000923 Title A name given to the resource Film script for Saturn C-1/C-1B quarterly film report no. 13 (covering July, August, September, 1962). Description An account of the resource Film script reporting on how the Saturn 1 will be used and what its take-off process will look like Date A point or period of time associated with an event in the lifecycle of the resource 1963-01-01 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Saturn project Saturn launch vehicles--Design and construction Saturn launch vehicles--Testing Saturn 1 launch vehicles Type The nature or genre of the resource Text Film Scripts Source A related resource from which the described resource is derived Saturn V Collection University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama Is Part Of A related resource in which the described resource is physically or logically included. Is part of: Uprated Saturn IB quarterly film reports and related material #9, 10, 11, 12, 13, 14, 15, 16, 17, 18. 8/2TMRF. Language A language of the resource en Rights Information about rights held in and over the resource This material may be protected under U. S. Copyright Law (Title 17, U.S. Code) which governs the making of photocopies or reproductions of copyrighted materials. You may use the digitized material for private study, scholarship, or research. Though the University of Alabama in Huntsville Archives and Special Collections has physical ownership of the material in its collections, in some cases we may not own the copyright to the material. It is the patron's obligation to determine and satisfy copyright restrictions when publishing or otherwise distributing materials found in our collections. Relation A related resource spc_stnv_000900_000924 https://digitalprojects.uah.edu/files/original/20/10291/uprsatIBquafilrepandrelmatfilsciforsatquafilrepno10_071007101257.pdf 32e8c5eacf2113fee9630e3aaabf99ab Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Title A name given to the resource Saturn V Collection Relation A related resource <a href="http://libarchstor.uah.edu:8081/repositories/2/resources/60" target="_blank" rel="noreferrer noopener">View the Saturn V Collection finding aid in ArchivesSpace</a> Identifier An unambiguous reference to the resource within a given context Saturn V Collection Description An account of the resource <p>The Saturn V was a three-stage launch vehicle and the rocket that put man on the moon. (Detailed information about the Saturn V's three stages may be found<span> </span><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_first_stage.html">here,<span> </span></a><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_second_stage.html">here,<span> </span></a>and<span> </span><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_third_stage.html">here.</a>) Wernher von Braun led the Saturn V team, serving as chief architect for the rocket.</p> <p>Perhaps the Saturn V’s greatest claim to fame is the Apollo Program, specifically Apollo 11. Several manned and unmanned missions that tested the rocket preceded the Apollo 11 launch. Apollo 11 was the United States’ ultimate victory in the space race with the Soviet Union; the spacecraft successfully landed on the moon, and its crew members were the first men in history to set foot on Earth’s rocky satellite.</p> <p>A Saturn V rocket also put Skylab into orbit in 1973. A total of 15 Saturn Vs were built, but only 13 of those were used.</p> Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context uprsatIBquafilrepandrelmatfilsciforsatquafilrepno10_071007101257.pdf spc_stnv_000920 Title A name given to the resource Film script for Saturn quarterly film report no. 10 (covering October, November, December, 1961). Description An account of the resource Film script reporting on the construction of the Saturn 1 Date A point or period of time associated with an event in the lifecycle of the resource 1962-01-01 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Saturn project Saturn launch vehicles--Design and construction Type The nature or genre of the resource Text Film Scripts Source A related resource from which the described resource is derived Saturn V Collection University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama Is Part Of A related resource in which the described resource is physically or logically included. Is part of: Uprated Saturn IB quarterly film reports and related material #9, 10, 11, 12, 13, 14, 15, 16, 17, 18. 8/2TMRF. Language A language of the resource en Rights Information about rights held in and over the resource This material may be protected under U. S. Copyright Law (Title 17, U.S. Code) which governs the making of photocopies or reproductions of copyrighted materials. You may use the digitized material for private study, scholarship, or research. Though the University of Alabama in Huntsville Archives and Special Collections has physical ownership of the material in its collections, in some cases we may not own the copyright to the material. It is the patron's obligation to determine and satisfy copyright restrictions when publishing or otherwise distributing materials found in our collections. Relation A related resource spc_stnv_000900_000924 https://digitalprojects.uah.edu/files/original/20/10292/uprsatIBquafilrepandrelmatfilsciforsatquafilrepno11_071007101814.pdf cdc0cd3905b1fbd338aaadaaaf330799 Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Title A name given to the resource Saturn V Collection Relation A related resource <a href="http://libarchstor.uah.edu:8081/repositories/2/resources/60" target="_blank" rel="noreferrer noopener">View the Saturn V Collection finding aid in ArchivesSpace</a> Identifier An unambiguous reference to the resource within a given context Saturn V Collection Description An account of the resource <p>The Saturn V was a three-stage launch vehicle and the rocket that put man on the moon. (Detailed information about the Saturn V's three stages may be found<span> </span><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_first_stage.html">here,<span> </span></a><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_second_stage.html">here,<span> </span></a>and<span> </span><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_third_stage.html">here.</a>) Wernher von Braun led the Saturn V team, serving as chief architect for the rocket.</p> <p>Perhaps the Saturn V’s greatest claim to fame is the Apollo Program, specifically Apollo 11. Several manned and unmanned missions that tested the rocket preceded the Apollo 11 launch. Apollo 11 was the United States’ ultimate victory in the space race with the Soviet Union; the spacecraft successfully landed on the moon, and its crew members were the first men in history to set foot on Earth’s rocky satellite.</p> <p>A Saturn V rocket also put Skylab into orbit in 1973. A total of 15 Saturn Vs were built, but only 13 of those were used.</p> Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context uprsatIBquafilrepandrelmatfilsciforsatquafilrepno11_071007101814.pdf spc_stnv_000921 Title A name given to the resource Film script for Saturn quarterly film report no. 11 (covering January, February, March, 1962). Description An account of the resource Film script reporting on the construction of the Saturn 1 Date A point or period of time associated with an event in the lifecycle of the resource 1963-01-01 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Saturn project Saturn launch vehicles--Design and construction Type The nature or genre of the resource Text Film Scripts Source A related resource from which the described resource is derived Saturn V Collection University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama Is Part Of A related resource in which the described resource is physically or logically included. Is part of: Uprated Saturn IB quarterly film reports and related material #9, 10, 11, 12, 13, 14, 15, 16, 17, 18. 8/2TMRF. Language A language of the resource en Rights Information about rights held in and over the resource This material may be protected under U. S. Copyright Law (Title 17, U.S. Code) which governs the making of photocopies or reproductions of copyrighted materials. You may use the digitized material for private study, scholarship, or research. Though the University of Alabama in Huntsville Archives and Special Collections has physical ownership of the material in its collections, in some cases we may not own the copyright to the material. It is the patron's obligation to determine and satisfy copyright restrictions when publishing or otherwise distributing materials found in our collections. Relation A related resource spc_stnv_000900_000924 https://digitalprojects.uah.edu/files/original/20/10293/uprsatIBquafilrepandrelmatfilsciforsatquafilrepno12_071007102253.pdf 843c32967538ad77b0c52c8644519679 Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Title A name given to the resource Saturn V Collection Relation A related resource <a href="http://libarchstor.uah.edu:8081/repositories/2/resources/60" target="_blank" rel="noreferrer noopener">View the Saturn V Collection finding aid in ArchivesSpace</a> Identifier An unambiguous reference to the resource within a given context Saturn V Collection Description An account of the resource <p>The Saturn V was a three-stage launch vehicle and the rocket that put man on the moon. (Detailed information about the Saturn V's three stages may be found<span> </span><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_first_stage.html">here,<span> </span></a><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_second_stage.html">here,<span> </span></a>and<span> </span><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_third_stage.html">here.</a>) Wernher von Braun led the Saturn V team, serving as chief architect for the rocket.</p> <p>Perhaps the Saturn V’s greatest claim to fame is the Apollo Program, specifically Apollo 11. Several manned and unmanned missions that tested the rocket preceded the Apollo 11 launch. Apollo 11 was the United States’ ultimate victory in the space race with the Soviet Union; the spacecraft successfully landed on the moon, and its crew members were the first men in history to set foot on Earth’s rocky satellite.</p> <p>A Saturn V rocket also put Skylab into orbit in 1973. A total of 15 Saturn Vs were built, but only 13 of those were used.</p> Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context uprsatIBquafilrepandrelmatfilsciforsatquafilrepno12_071007102253.pdf spc_stnv_000922 Title A name given to the resource Film script for Saturn quarterly film report no. 12 (covering April, May, June, 1962). Description An account of the resource Film script reporting on the testing of the Saturn 1 Date A point or period of time associated with an event in the lifecycle of the resource 1963-01-01 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Saturn project Saturn launch vehicles--Design and construction Saturn launch vehicles--Testing Type The nature or genre of the resource Text Film Scripts Source A related resource from which the described resource is derived Saturn V Collection University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama Is Part Of A related resource in which the described resource is physically or logically included. Is part of: Uprated Saturn IB quarterly film reports and related material #9, 10, 11, 12, 13, 14, 15, 16, 17, 18. 8/2TMRF. Language A language of the resource en Rights Information about rights held in and over the resource This material may be protected under U. S. Copyright Law (Title 17, U.S. Code) which governs the making of photocopies or reproductions of copyrighted materials. You may use the digitized material for private study, scholarship, or research. Though the University of Alabama in Huntsville Archives and Special Collections has physical ownership of the material in its collections, in some cases we may not own the copyright to the material. It is the patron's obligation to determine and satisfy copyright restrictions when publishing or otherwise distributing materials found in our collections. Relation A related resource spc_stnv_000900_000924 https://digitalprojects.uah.edu/files/original/20/10290/uprsatIBquafilrepandrelmatfilsciforsatquafilrepno09_071007100203.pdf 8d475280aa264d2285b6556deec0686c Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Title A name given to the resource Saturn V Collection Relation A related resource <a href="http://libarchstor.uah.edu:8081/repositories/2/resources/60" target="_blank" rel="noreferrer noopener">View the Saturn V Collection finding aid in ArchivesSpace</a> Identifier An unambiguous reference to the resource within a given context Saturn V Collection Description An account of the resource <p>The Saturn V was a three-stage launch vehicle and the rocket that put man on the moon. (Detailed information about the Saturn V's three stages may be found<span> </span><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_first_stage.html">here,<span> </span></a><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_second_stage.html">here,<span> </span></a>and<span> </span><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_third_stage.html">here.</a>) Wernher von Braun led the Saturn V team, serving as chief architect for the rocket.</p> <p>Perhaps the Saturn V’s greatest claim to fame is the Apollo Program, specifically Apollo 11. Several manned and unmanned missions that tested the rocket preceded the Apollo 11 launch. Apollo 11 was the United States’ ultimate victory in the space race with the Soviet Union; the spacecraft successfully landed on the moon, and its crew members were the first men in history to set foot on Earth’s rocky satellite.</p> <p>A Saturn V rocket also put Skylab into orbit in 1973. A total of 15 Saturn Vs were built, but only 13 of those were used.</p> Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context uprsatIBquafilrepandrelmatfilsciforsatquafilrepno09_071007100203.pdf spc_stnv_000919 Title A name given to the resource Film script for Saturn quarterly film report no. 9 covering July, August, September, 1961. Description An account of the resource Film script reporting on the construction of the Saturn 1 Date A point or period of time associated with an event in the lifecycle of the resource 1962-01-01 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Saturn project Saturn launch vehicles--Design and construction Type The nature or genre of the resource Text Film Scripts Source A related resource from which the described resource is derived Saturn V Collection University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama Is Part Of A related resource in which the described resource is physically or logically included. Is part of: Uprated Saturn IB quarterly film reports and related material #9, 10, 11, 12, 13, 14, 15, 16, 17, 18. 8/2TMRF. Language A language of the resource en Rights Information about rights held in and over the resource This material may be protected under U. S. Copyright Law (Title 17, U.S. Code) which governs the making of photocopies or reproductions of copyrighted materials. You may use the digitized material for private study, scholarship, or research. Though the University of Alabama in Huntsville Archives and Special Collections has physical ownership of the material in its collections, in some cases we may not own the copyright to the material. It is the patron's obligation to determine and satisfy copyright restrictions when publishing or otherwise distributing materials found in our collections. Relation A related resource spc_stnv_000900_000924 https://digitalprojects.uah.edu/files/original/20/1156/spc_stnv_000072.pdf 2ec7547066c97c2fd55fea4efa5420fd PDF Text Text ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............. .......................... ............ ............. ............ ............... . N A T I O N A L A E R O N A U T I C S A N D SPACE ADMINISTRATIO ............................. .......... .:..,. . . .,&:.:.:.:.:.:.:.:.: . i.x:.:.:.:.:.:.:.:.:. ..................... ............ ............. FINAL ;;,. ..,........... ............. ..., .... .;. ..&:::::::: ...................... . . . . . . . . .SATURN I-IISTORY CCCUMENT .......... ................... . . ............. . .............. . . . . . . . ...... Universi~yof: Alabcma Ec :.-arch !nstitute 1 - a .:- !<j.%.:.:.:.:.:.:.:.:. History of Science C. Tecl..nofcgy Group .., . ?.-.~.-.~.~.~.~.~.~.~.~ . ,;-:*.:.:.:.:.;.;.:.:.:.:.:. ..... .i' ............... * ........... Date --- - - - - - - - Doc. No. - - - ----........... ............ ............. ............. ... ....,,. . .!<' ........... ..... ...*....-.m...-.*.*,-.-...-.-. c.;: .. .*;:+:.::.>>:.:.:.:. +:.-......: ............. .:?........::... . ............................. ............ .................. ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ PREPARED BY ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ LUNAR SURFACE OPERATIONS 0 FFICE ........... ............ ........... ............ ........... ............ ........... MISSION OPERATI.0NS BRANCH ............ ........... ............ ........... ............ ........... ............ ........... FLIGHT CREW SUPPORT DIVISION ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ JUNE 27,1969 ........... ............ ........... ............ ........... < ., : . , 11;';. , ,: a : , , . ', '. x .$., ~ *.~,:t.: ; . I + ,,,,---,, APOLLO 11 LUNAR SURFACE OPERATIONS PLAN M A N N E D SPACECRAFT C E N 1 HOUSTON.TEXAS ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... �FINAL EDITION APOLLO I1 LUNAR SURFACE OPERATIONS PLAN JUNE 13, 1969 Prepared by : w.. H . Wood, Jr. Lunar Surface operatio$. Off i c e Approved by : Lunar surflace Operations Off i c e H . A. Kuehnel Chief, Mission Operations Branch - C. H . Woodling \ \ Assistant Chief f o r Crew'Tra3,ning Chief, fight brew Support Division S~c33 k -. U ... . - Donald K . Slayton /\ Director of Flight( c ew Operations - -3 �APOLLO 11 LUNAR SURFACE OPERATIONS PLAN (FINAL EDITION) PREFACE This document h a s been prepared by t h e F l i g h t Crew Support D i v i s i o n , F l i g h t Crew Operations D i r e c t o r a t e , Manned S p a c e c r a f t C e n t e r , Houston, Texas. The i n f o r m a t i o n contained w i t h i n t h i s document r e p r e s e n t s t h e Lunar S u r f a c e Operations P l a n f o r Ap0110'11, t h e f i r s t planned l u n a r landing m i s s ion. T h i s i s t h e f i n a l e d i t i o n of t h e Apollo 11 Lunar S u r f a c e Operations P l a n . The p l a n i s under t h e c o n f i g u r a t i o n c o n t r o l of t h e Crew Procedures Control Board (CPCB) and a l l proposed changes t o t h i s document should b e submitted t o t h e CPCB v i a a Crew Procedures Change Request. Changes and comments t o t h e p l a n should b e d i r e c t e d t o W. H. Wood, Jr., Lunar S u r f a c e Operations O f f i c e , FCSD. �CONTENTS Page Preface iii L i s t of F i g u r e s and Tables vii 1.0 INTRODUCTION 1 2.0 MISSION PLAN 2.1 2.2 2.3 3.0 Mission Mission Summary 2.3.1 2.3.2 Purpose Description of Mission Requirements Introduction Mission Objectives and Experiments NOMINAL LUNAR EVA 3.1 3.2 3.3 3.4 3.5 Timeline D e s c r i p t i o n and R a t i o n a l e 3.1.1 Lunar Surface Stay 3.1.2 Extravehicular Activity Task and Data D e s c r i p t i o n s 3.2.1 Environmental F a m i l i a r i z a t i o n 3.2.2 Preliminary Checks 3.2.3 T e l e v i s i o n Coverage 3.2.4 S-band E r e c t a b l e Antenna Deployment 3.2.5 Photography 3.2.6 EVA and Environment E v a l u a t i o n 3.2.7 Sample C o l l e c t i o n s 3.2.8 LM I n s p e c t i o n 3.2.9 Experiment Deployments 3.2.10 Use of Lunar Equipment Conveyor 3.2.11 EVA Termination Summary Timeline Timeline D e t a i l e d Procedures 3.5.1 Nominal A c t i v i t i e s Sequence 3.5.2 Procedures �ALTERNATE AND CONTINGENT PLANS 4.1 4.2 4.3 A l t e r n a t e EVA (With S-band E r e c t a b l e Antenna ~ e p l o y m e n t ) 4.1.1 D e s c r i p t i o n and R a t i o n a l e 4.1.2 Summary T i m e l i n e 4.1.3 Timeline 4.1.4 D e t a i l e d Procedures C o n t i n g e n t EVA 1-Minimum Time, One Man 4.2.1 D e s c r i p t i o n and R a t i o n a l e 4.2.2 Summary T i m e l i n e 4.2.3 Timeline C o n t i n g e n t EVA 2-One Man, Two Hours 4.3.1 D e s c r i p t i o n and R a t i o n a l e 4.3.2 Summary T i m e l i n e 4.3.3 Timeline APPENDIX 5.1 5.2 5.3 5.4 5.5 Abbreviations D e t a i l e d O b j e c t i v e s and Experiments 5.2.1 Introduction 5.2.2 Definitions 5.2.3' Objectives 5.2.4 Experiments Lunar S u r f a c e O p e r a t i o n a l C o n s t r a i n t s 5.3.1 Introduction 5.3.2 Constraints Classification 5.3.2.1 Constraint Categories 5.3.2.2 Violation Classification 5.3.3 Mission O p e r a t i o n s C o n s t r a i n t s 5.3.4 Lunar S u r f a c e O p e r a t i o n s C o n s t r a i n t s 5.3.5 Equipment O p e r a t i o n C o n s t r a i n t s 5.3.6. Equipment Design C o n s t r a i n t s 5.3.7 General C o n s t r a i n t s Nominal Lunar S u r f a c e EVA M e t a b o l i c P r o f i l e s 5.4.1 Introduction 5.4.2 CDR M e t a b o l i c P r o f i l e 5.4.3 LMP M e t a b o l i c P r o f i l e References PAGE �FIGURES Figure Number Title Lunar s u r f a c e a c t i v i t y t i m e l i n e f o r 22-hour s t a y Radar coverage during l u n a r . s t a y f o r launch d a t e of J u l y 16 . TV f i e l d of view from MESA TV f i e l d of view from t r i p o d (with Lunar Day lens) Quad I i n s p e c t i o n p o i n t s Quad I1 i n s p e c t i o n p o i n t s Quad 111 i n s p e c t i o n p o i n t s Quad I V i n s p e c t i o n p o i n t s Probable a r e a s f o r l u n a r s u r f a c e a c t i v i t y TABLES Table No. 3- 1 Performance margins f o r LM communications 3-2 Loose equipment l e f t on l u n a r s u r f a c e vii Page , 12 �SECTION 1.0 INTRODUCTION �1.0 INTRODUCTION This final edition of the Lunar Surface Operations'Plan defines equipment requirements, crewlequipment interfaces, and final flight planning and crew activities for lunar surface EVA operations during the first manned lunar landing mission. This plan delineates how the lunar surface operational and scientific objectives for the first manned lunar landing mission will be accomplished through pre-mission timelining and procedures definition. Although the primary concern of this plan is the lunar surface EVA operational aspects of the mission, interface relationships are presented to provide clarity and continuity to the overall mission plan. The nominal plan is for a single two-man lunar excursion. The planned duration will be two hours and forty minutes or upon reaching a pre-determined red line on one of the PLSS consumable~. The red line is defined as having either a 30 minute supply of oxygen or a 30 minute supply of feedwater remaining after repressurization. The battery is not considered to be a constraint on the lunar surface time for this mission. Based on an estimation of each crewman's BTU expenditure to accomplish his respective EVA tasks, a PLSS expendable red line should not be reached during the EVA. The Commander is expected to expead approximately 3625 BTU's which will leave a 1175 BTU PLSS reserve or approximately 50 minutes Lunar surface time. (Metabolic profiles are presented in the Appendix, Section 5.4) In addition to the nominal timeline, the plan presents three other timelines for the lunar EVA. One timeline is referred to as an alternate timeline and two are referred to as contingent timelines. These timelines differ from the nominal primarily by additions or deletions of tasks. The major difference in the alternate timeline, from the nominal, is the addition of the S-band erectable antenna deployment which reduces the time available for the documented sample collection. The first contingent timeline, Contingent EVA 1, is a presentation of activities for a minimum-time, one-man EVA. The second contingent timeline, Contingent EVA 2, is for a one-man, two-hour EVA. . �The p l a n a l s o p r e s e n t s two forms of t i m e l i n e s . The l i n e s and a t i m e l i n e f o r t h e complete l u n a r s u r f a c e touchdown t o l i f t o f f , a r e i n summary form. Each of t i m e l i n e s i s a l s o p r e s e n t e d i n an expanded t i m e l i n e v i a t e d procedures form. EVA times t a y , from t h e EVA and abbre- D e t a i l e d procedures a r e included f o r t h e nominal l u n a r EVA. S i n c e t h e a l t e r n a t e t i m e l i n e , i n g e n e r a l , only adds t h e deployment of t h e e r e c t a b l e antenna and reduces t h e time f o r c o l l e c t i o n of a documented sample, d e t a i l e d procedures f o r t h e e n t i r e a l t e r n a t e EVA would b e redundant. Thus, only d e t a i l e d procedures f o r t h e S-band e r e c t a b l e antenna deployment a r e included. For t h e c o n t i n g e n t EVA'S, t h e t i m e l i n e s p r e s e n t t h e procedures i n s u f f i c i e n t d e t a i l t h a t , with a n understanding o r r e f e r e n c e t o t h e nominal procedures, s e p a r a t e procedures a r e unnecessary. �SECTION 2.0 MISSION PLAN �MISSION PLAN Mission Purpose The primary purpose of t h e Apollo 11 mission i s t ~ ' ~ e r f o r m a manned l u n a r landing and r e t u r n . Subordinate o b j e c t i v e s a r e t o perform l i m i t e d s e l e n o l o g i c a l i n s p e c t i o n , photography, survey, e v a l u a t i o n , and sampling during t h e l u n a r s t a y . Data w i l l b e obtained t o a s s e s s t h e c a p a b i l i t y and l i m i t a t i o n s of t h e a s t r o n a u t and h i s equipment i n t h e l u n a r environment. The accomplishment of t h e d e t a i l e d l u n a r s u r f a c e mission' o b j e c t i v e s and experiments w i l l c o n t r i b u t e a n e s s e n t i a l p a r. t . t o t h e success of t h e mission. 2.2 Mission Description This s e c t i o n provides a b r i e f summary of t h e major events f o r a J u l y 16, 1969 launch date. Launch t o Earth Orbit: The J u l y 16 mission w i l l allow a range of launch azimuths from 72 t o 108 degrees with a window opening a t 13:32:00 The s p a c e c r a f t (hr:min:sec) gmt f o r a d u r a t i o n of 4:24:00. w i l l b e i n s e r t e d i n t o an approximately 100 n a u t i c a l m i l e c i r c u l a r e a r t h parking o r b i t f o r s p a c e c r a f t checkout. Translunar I n j e c t i o n (TLI) : The J u l y window permits a P a c i f i c t r a n s l u n a r i n j e c t i o n . The S-IVB w i l l b e re-ignited during t h e second e a r t h p a r k i n g o r b i t t o provide t h e nominal i n j e c t i o n . Translunar Coast: Two hours a f t e r TLI, t h e CSM w i l l s e p a r a t e from t h e S-IV, transpose, dock and i n i t i a t e e j e c t i o n of t h e LM/CSM. P r i o r t o l u n a r o r b i t i n s e r t i o n (LOI), two a s t r o n a u t s w i l l e n t e r t h e LM, accomplish a l i m i t e d s t a t u s check, and r e t u r n t o t h e command module. �Lunar Orbit Insertion: The service module propulsion system will insert the spacecraft into an orbit of approximately 60 by 170 nautical miles. After two revolutions in this orbit for spacecraft system and orbit parameter checks, the orbit will be reduced to 66 by 54 nautical miles.. Lunar Module Descent: During the thirteenth orbit after the Lunar Orbit ~nsertion, LM/CSM undocking is accomplished in preparation for lunar landing. The powered descent maneuver is initialized at pericynthion of the descent transfer orbit. For the July 16 launch, the lunar landing will be at Site 2 (previously designated 11-P-6 and located at 0" 43' N, 23" 42' E). The range of sun elevation angles, for landing, will be from 10.5 to 13.5 degrees. Lunar Surface Operations: The planned lunar surface staytime is 22 hours. The nominal plan provides for a single, two-man EVA, with a duration of two hours and forty minutes. . . . Immediately after landing, the LM will be checked to assess its launch capability. After the post-landing checks, there will be a four hour rest period, with eat periods before and after, prior to preparation for EVA. Following the EVA and post-EVA activities, there will be another rest period, of four hours and forty minutes duration, prior to preparation for liftoff. In addition to the tasks required to successfully complete the landing and.ascent and the pre-EVA and post-EVA operations, the lunar surface activities will include the following major items in order of priority: 1) Photographs of the landing area through the LM cabin window. 2) Contingency sample collection. �3) EVA e v a l u a t i o n . 4) LM i n s p e c t i o n . 5) Bulk sample c o l l e c t i o n . 6) Deployment of experiments : Early Apollo . S c i e n t i f i c Experiments Package (S-031, Lunar P a s s i v e Seismology and S-078, Laser Ranging Retro-Reflector) and S-080, S o l a r Wind Composition. 7) Documented sample c o l l e c t i o n . Real time TV coverage w i l l b e provided e a r l y i n t h e EVA u s i n g t h e s t e e r a b l e antenna o r , i f r e q u i r e d , t h e e r e c t a b l e antenna. Both t h e Goldstone and Parkes 210-foot antennas w i l l b e u t i l i z e d as a v a i l a b l e . Photography w i l l b e employed throughout t h e EVA t o document t h e a c t i v i t i e s and o b s e r v a t i o n s . LM A s c e n t : During t h e LM l u n a r s u r f a c e s t a y , t h e CSM w i l l make t h e r e q u i r e d p l a n e change t o permit a nominally coplanar rendezvous. A f t e r LM a s c e n t and docking t o t h e CSM, t h e two crewmen w i l l t r a n s f e r t o t h e CSM w i t h exposed f i l m and samples of t h e l u n a r s u r f a c e . The CSM w i l l then j e t t i s o n t h e LM u s i n g t h e SM RCS. Transearth Injection: The s e r v i c e module p r o p u l s i o n system w i l l b e used t o b o o s t t h e CSM o u t of l u n a r o r b i t . The r e t u r n f l i g h t d u r a t i o n s h a l l n o t exceed 110 hours and t h e r e t u r n i n c l i n a t i o n s h a l l n o t exceed 40 degrees. Entry and Recovery: P r i o r t o atmospheric e n t r y , t h e command module w i l l b e s e p a r a t e d from t h e s e r v i c e module u s i n g t h e SM RCS. The nominal range from 400,000 f e e t a l t i t u d e t o touchdown s h a l l b e 1285 n a u t i c a l miles.. Touchdown w i l l be i n t h e P a c i f i c n e a r Hawaii approximately 11 days a f t e r launch from e a r t h . �P o s t Landing Operations: Following splashdown, t h e crew w i l l e g r e s s t h e CM a f t e r t h e f l o t a t i o n c o l l a r h a s been a t t a c h e d , don b i o l o g i c a l i s o l a t i o n garments, t r a n s f e r t o t h e recovery s h i p by h e l i c o p t e r and immediately e n t e r t h e Mobile Quarantine F a c i l i t y (MQF) They w i l l b e t r a n s p o r t e d i n t h e MQF t o t h e LRL a t MSC. The CM, sample r e t u r n c o n t a i n e r s , f i l m , t a p e s and a s t r o n a u t l o g s w i l l a l s o b e t r a n s p o r t e d t o t h e LRL. . I n o r d e r t o minimize t h e r i s k of contamination of t h e e a r t h ' s b i o s p h e r e by l u n a r m a t e r i a l , q u a r a n t i n e measures w i l l b e enforced. The crew w i l l b e q u a r a n t i n e d f o r approximately 2 1 days a f t e r l i f t o f f from t h e l u n a r s u r f a c e . 2.3 Summary of Mission Requirements 2.3.1 Introduction The f o l l o w i n g i n f o r m a t i o n i s from t h e "Mission Requirements SA-506lCSM-107lLM-5 G Type Mission, Lunar Landing", Dated A p r i l 17, 1969. (Revised May 1, 1969) The f o l l o w i n g s i n g l e primary mission o b j e c t i v e i s a s s i g n e d t o t h i s . m i s s i o n by t h e O f f i c e of Manned Space F l i g h t (OMSF): 1) Perform manned l u n a r l a n d i n g and r e t u r n . I n a d d i t i o n , t h e f o l l o w i n g s u b o r d i n a t e o b j e c t i v e s a r e del i n a t e d by OMSF: 1) P e r f orm s e l e n o l o g i c a l i n s p e c t i o n and sampling. 2) Obtain d a t a t o a s s e s s t h e c a p a b i l i t y and l i m i t a t i o n s of t h e a s t r o n a u t and h i s equipment i n t h e l u n a r s u r f a c e environment. F i n a l l y , t h e f o l l o w i n g experiments have been a s s i g n e d t o t h i s mission: 1) S-031 Lunar P a s s i v e Seismology 2) S-078 L a s e r Ranging Retro-Reflector �. . 3) S-080 S o l a r Wind Composition 4) S-151 Cosmic Ray Detection 5) T-029 P i l o t Describing Function . . . . . The Mission Requirements document i n c o r p o r a t e s t h e s e v a r i o u s o b j e c t i v e s and experiments, d e t a i l s them where necessary, and places them i n t h e proper order of p r i o r i t y , thereby providing t h e l e v e l of d e t a i l necessary f o r mission planning. The document n o t e s , however, t h a t : . There a r e no Detailed Objectives, a s such, which have been derived from t h e primary o b j e c t i v e of "perform manned l u n a r landing and return"., D e t a i l e d Objectives have, however, been derived from t h e two OMSF subordinate o b j e c t i v e s . The mission w i l l b e flown as an o p e r a t i o n a l mission i n t h e sense t h a t i t w i l l b e performed i n t h e most expeditious manner p o s s i b l e with no i n t e r f e r e n c e from s p e c i a l tests o r operations which a r e n o t necessary f o r t h e performance of t h i s b a s i c o b j e c t i v e . The manner i n which t h e detailed.performance of t h i s o b j e c t i v e i s met w i l l be contained i n t h e Mission Report. 2) Experiments a r e d e t a i l e d and p r i o r i t i e d i n t h e requirements document only when they a r e such a s t o r e q u i r e some a c t i o n by t h e crew o r otherwise impact t h e timeline. Thus, t h e Cosmic Ray Detection experiment, S-151, a passive experiment l i m i t e d t o p o s t mission a n a l y s i s of t h e f l i g h t helmets, is only mentioned and does n o t appear i n t h e p r i o r i t y list o r a s a detailed objective. S i m i l a r l y , ' t h e P i l o t Describing Function experiment, T-029, only r e q u i r e s c e r t a i n p o r t i o n s of voice and telemetry d a t a recordings and does n o t appear i n t h e l i s t of o b j e c t i v e s and experiments. The Detailed Objectives f o r t h e f i r s t l u n a r landing mission w i l l b e o b j e c t i v e s which concern equipment and crew o p e r a t i o n s only during t h e l u n a r surf ace phase of t h e mission. The c a p a b i l i t y t o s u c c e s s f u l l y complete o t h e r mission phases w i l l have been demonstrated on p r i o r missions. �Mission O b j e c t i v e s and Experiments .The f o l l o w i n g summary of l u n a r EVA o b j e c t i v e s and experiments i s i n o r d e r of p r i o r i t y , w i t h t h e o b j e c t i v e o r experiment of h i g h e s t p r i o r i t y l i s t e d f i r s t . The o r d e r of p r i o r i t y i s based upon t h e r e l a t i v e importance t o t h e Apollo s p a c e c r a f t development program o r t o t h e advancement of l u n a r s c i e n c e . The D e t a i l e d O b j e c t i v e s and Experiments a r e i n c l u d e d i n t h e Appendix, S e c t i o n 5.2. The o b j e c t i v e s " T e l e v i s i o n Coverage" and "Photographic Coverage" w i l l b e performed i n c o n j u n c t i o n w i t h s e v e r a l of t h e o t h e r obj e c t i v e s o r experiments. The a s s o c i a t e d o p e r a t i o n s w i l l t a k e p l a c e a t v a r i o u s p o i n t s i n t h e t i m e l i n e . Hence, t h e s e two ' o b j e c t i v e s cannot b e a s s i g n e d any s p e c i f i c p r i o r i t y i n t h e l i s t below and a r e t h e r e f o r e i n c l u d e d a t t h e end. Priority O b j e c t i v e s and Experiments 1 A Contingency Sample C o l l e c t i o n B Lunar S u r f a c e EVA Operations 3 C EMU Lunar Surface Operations 4 D Landing E f f e c t s on LM 5 E Lunar S u r f a c e C h a r a c t e r i s t i c s 6 F Bulk Sample C o l l e c t i o n 7 G Landed LM Location 8 H Lunar Environment V i s i b i l i t y 9 I Assessment of Contamination by Lunar M a t e r i a l 10 S-031 Lunar P a s s i v e Seismology 11 S-078 Laser Ranging Retro-Reflector 12 S-080 S o l a r Wind Composition �J Documented Sample C o l l e c t i o n K (Included i n Photographic Coverage, Change A, May 1, 1969) L T e l e v i s i o n Coverage M Photographic Coverage �SECTION 3.0 NOMINAL LUNAR EVA �' . 3.0 NOMINAL LUNAR EVA 3.1 Timeline D e s c r i p t i o n and Rationale 3.1.1 Lunar Surface Stay The nominal plan i s f o r two crewmen, t h e Commander and t h e Lunar Module P i l o t , t o remain on t h e l u n a r s u r f a c e f o r approximately 22 hours. During t h i s period, the'crew w i l l accomplish postlanding and pre-ascent procedures and e x t r a v e h i c u l a r a c t i v i t y . There w i l l be two r e s t and s e v e r a l e a t periods. A timeline f o r t h e l u n a r s u r f a c e s t a y i s presented i n Figure 3-1. There a r e s e v e r a l c o n s i d e r a t i o n s which a r e t h e b a s i s f o r t h e sequence of a c t i v i t y f o r t h e l u n a r s u r f a c e s t a y . An e a r l y r e s t peiod i s planned which w i l l provide r e s t b e f o r e t h e strenuous pre-EVA, EVA, and post-EVA a c t i v i t i e s and i n s u r e t h e work day i s n o t p r o h i b i t i v e l y long i f l i f t o f f i s req u i r e d b e f o r e t h e o t h e r planned r e s t period. A second r e s t p e r i o d of f o u r hours and f o r t y minutes i s provided a f t e r t h e EVA b e f o r e t h e c r u c i a l l i f t o f f and rendezvous sequence. 3.1.2 - Extravehicular A c t i v i t y The f i r s t l u n a r EVA i s designed t o maximize t h e r e t u r n of s c i e n t i f i c and o p e r a t i o n a l data. However, t h e t i m e l i n e permits r e s t periods and a gradual i n c r e a s e i n t a s k complexity w i t h simple t a s k s i n i t i a l l y f o r crew acclimation and PLSS-EMU data analysis. There w i l l be two major a r e a s of e v a l u a t i o n during t h e l u n a r s u r f a c e EVA. The f i r s t concern i s with comprehensive crew f a m i l i a r i z a t i o n and e v a l u a t i o n of EVA c a p a b i l i t y and t h e l u n a r environment. The i n v e s t i g a t i o n w i l l b e a methodical approach which w i l l enhance t h e accomplishment of t h i s EVA a s w e l l a s demonstrate a s t r o n a u t and equipment c a p a b i l i t y f o r f u t u r e l u n a r s u r f a c e e x p l o r a t i o n . The second a r e a is t h e c o l l e c t i o n of o p e r a t i o n a l and s c i e n t i f i c data. The a n a l y s i s of t h i s d a t a w i l l a s s i s t i n t h e update of equipment designs a s ' w e l l a s i n c r e a s e our general understanding of t h e l u n a r s u r f a c e . The f i r s t few minutes of t h e EVA; t h e Lunar Module P i l o t (LMP) w i l l remain i n s i d e t h e LM a s c e n t s t a g e t o monitor t h e Commander's (CDR) s u r f a c e a c t i v i t y and t h e LM systems i n t h e �' depressurized state. The CDR will descend to the lunai surface to conduct several preliminary tasks. He will determine . his ability to operate in the lunar environment; collect a contingency lunar sample and take still color photographs (with an electric 70mm camera) as he checks the LM . and the lunar surface condition which affect the accomplishment of the EVA tasks. In addition to the TV coverage and still photographs, the LMP can visually observe and obtain sequence camera (data acquistiion) coverage to supplement the documentation of the CDR activity. With only one crewman on the surface during the first few minutes of the EVA, a more effective PLSS telemetry data analysis can be conducted. The real time use rate for the PLSS consumables will be compared with the predicted rate to determine the PLSS capability for'EVAcontinuation. After the CDR accomplishes the preliminary EVA tasks, the LMF' will descend to the surface and spend a few minutes in the familiarization and evaluation of his capability or limitations to conduct further operations in the lunar environment. After this short period of time he will deploy the Solar Wind Composition (SWC) experiment. The CDR, after photographing the LMPts egress and descent to the surface, will remove the TV camera and tripod from the descent for stage modularized equipment stowage assembly (MESA) and move them to a position for optimum coverage of the subsequent surface EVA operations. Then, while the CDR collects a bulk sample of lunar surface material, the LMP will continue to become more familiar with his ability to operate in the lunar environment as he conducts the EVA and Environment Evaluation. The LMP begins the LM inspection and is joined by the CDR after the bulk sample has been collected. When the crewmen reach the scientific equipment (SEQ) bay in Quad 11, the LMP removes the Early Apollo Scientific Experiments Package (EASEP) as the CDR completes the LM inspection and photographically documents the LMP's activity. After they deploy the EASEP, the crew will select, describe, photograph, and collect samples until they terminate the EVA. In summary, there is a general increase in task complexity for both crewmen. The conservative timeline permits the crew to follow a slow, methodical approach in accomplishing each task. Additionally, the frequent rest periods within �Figure 3 - 1 rum scrlr )r,Ono f:LY."ct KCM !LY Q -;I -2 IM MRS. -13 w fZccml UIPOSKIIC V . 4 UI COYWLMEU k PILOT ACTIVITY <> T I M SCAlr IYHRS.-3 -:z 'I 0 A TO~W W N OYISIDI lWlNEml .C*ICKWI ~CO C II~C IV 4 w wurcff n s m n C l U L C10lI C M l W U l D l H A M 1 OI?RESS O e t t P L t E E W I P U f I l PC4 J E I I I S O I Y Y P L C CDLLECllm OREIIYIUtVCMCCIS . S d l l D I ~ 1 t I M D C I L O V Y I ~ l U L l E * M l E ISYC LINE1 O L Y I I#IlUL CVAA.OEWIOYEIl4L CAY. 01" .I0 s 1 C OIPLWY.1 OW. E I V l t O l f I1W U W I I O I .-LI Y Y I L E COLLCCIDI U I IISP(ClIO# .EASE, OCPLOVYE*I *XXUYE#lCO Y Y P L E ICM U I SUT I 111EGtllV .Jf111SOm EWI* ~ S l A B L I S *c.11" I.1ICtllV �LUNAR SURFACE ACTIVITY TIMELINE FOR 22 HOUR STAY 1 tuaw ! t I i t srArus cmm 1I WRM U CLfll 8 ?~~CWnWllW I 1 061VE GO $01 RE51 �t h e timeline add t o t h i s conservatism and i n s u r e t h a t each crewman and h i s PLSS remain i n a nominal o p e r a t i n g condition. However, should t h e EVA b e terminated a t any p o i n t i n t h e t i m e l i n e , t h e maximum d a t a r e t u r n f o r t h e t i m e spent on t h e . s u r f a c e w i l l be assured. Task and Data Descriptions Although t h e d e t a i l e d procedures d e s c r i b e t h e s t e p s t o ac- ,complish each t a s k , f u r t h e r explanation of t h e d e s i r e d d a t a and d a t a c o l l e c t i o n processes is d e s i r a b l e . 3.2.1 Environmental F a m i l i a r i z a t i o n A s mentioned previously, t h e t i m e l i n e considerations f o r t h e l u n a r s u r f a c e e x t r a v e h i c u l a r a c t i v i t y w i l l permit a slow buildup of t a s k complexity t o i n s u r e thorough crew f a m i l i a r i z a t i o n with t h e l u n a r environment y e t optimize t h e d a t a r e t u r n . The approach with which t h e crewmen w i l l proceed w i l l permit them t o adapt t o t h e environment while determining t h e ease o r d i f f i c u l t y which they can expect through o u t t h e EVA. The f i r s t crewman t o e g r e s s , a f t e r determining h i s i n i t i a l EVA c a p a b i l i t y , can a d v i s e t h e second crewman on what t o expect and possibly suggest methods t o accomplish t h e a d d i t i o n a l t a s k s . Both crewmen's experiences w i l l b e invaluable f o r p r e d i c t i n g crew c a p a b i l i t y on f u t u r e l u n a r s u r f a c e explorations. Once on t h e s u r f a c e , t h e CDR w i l l move slowly from t h e footpad t o check h i s balance and determine h i s a b i l i t y t o cont i n u e with t h e EVA--the a b i l i t y t o move and t o s e e o r , s p e c i f i c a l l y , t o perform t h e s u r f a c e operations w i t h i n t h e c o n s t r a i n t s of t h e EMU and t h e l u n a r environment. Although a more thorough e v a l u a t i o n and documentation of a.crewmanls c a p a b i l i t i e s w i l l occur l a t e r i n t h e timeline, t h i s i n i t i a l f a m i l i a r i z a t i o n w i l l a s s u r e t h e CDR t h a t h e and t h e LMP a r e capable of accomplishing t h e assigned EVA t a s k s . Also, should i t be necessary t o unexpectedly terminate t h e EVA p r i o r t o f u r t h e r environment evaluation, t h i s e a r l y famili a r i z a t i o n w i l l i n s u r e some d a t a r e t u r n on EVA c a p a b i l i t y and t h e l u n a r s u r f a c e p r o p e r t i e s . �. 3.2.2 . P r e l i m i n a r y Checks For t h e P r e l i m i n a r y Checks t h e CDR w i l l t r a n s f e r t h e 70mm . EL Data.camera t o t h e s u r f a c e , conduct a b r i e f LM check and a p r e l i m i n a r y e v a l u a t i o n of t h e l u n a r environment. The Hasselblad camera w i l l e n a b l e t h e CDR t o t a k e s t i l l c o l o r photographs t o supplement t h e sequence ( d a t a a c q u i s i t i o n ) camera photography which t h e LMP w i l l a t t a i n through t h e LM a s c e n t s t a g e window t o document.the s u r f a c e a c t i v i t y . A b r i e f check of t h e LM s t a t u s i s a simple t a s k which can b e used t o extend t h e CDR's environment f a m i l i a r i z a t i o n . and, a t t h e same time, p r o v i d e an important c o n t r i b u t i o n ' t o t h e p o s t f l i g h t assessment of t h e LM l a n d i n g should a . f u l l o r nominal LM i n s p e c t i o n n o t b e accomplished l a t e r . The p r e l i m i n a r y e v a l u a t i o n of t h e c o n d i t i o n s which w i l l . i n f l u e n c e t h e crewmen's s u r f a c e o p e r a t i o n s , such a s t h e t e r r a i n s u r f a c e f e a t u r e s and l i g h t i n g o r v i s i b i l i t y , w i l l a l s o enhance t h e CDR's environmental f a m i l i a r i z a t i o n 'as w e l l a s h i s assessment of an a s t r o n a u t ' s c a p a b i l i t y t o accomplish EVA t a s k s . From a p o s i t i o n n e a r t h e l a d d e r t h e CDR w i l l make a g e n e r a l i n s p e c t i o n of t h e LM and s u r f a c e about t h e LM. For t h e LM and s u r f a c e v i s i b l e t o him, h e w i l l b r i e f l y examine t h e g e a r s t r u t s , f o o t p a d s , and major p a r t s of t h e s p a c e c r a f t t o a s s u r e t h a t t h e LM i s s t a b l e and w i l l provide a s a f e o p e r a t i o n s b a s e f o r t h e l u n a r s t a y . An i n s p e c t i o n of t h e s u r f a c e w i l l prov i d e p r e l i m i n a r y d a t a on t h e LM e f f e c t on t h e s u r f a c e d u r i n g t h e landing. 3.2.3 TV Coverage The primary purpose of t h e TV i s t o provide a supplemental r e a l time d a t a s o u r c e t o a s s u r e o r enhance t h e s c i e n t i f i c and o p e r a t i o n a l d a t a r e t u r n . It may b e a n a i d i n d e t e r mining t h e e x a c t LM l o c a t i o n on t h e l u n a r s u r f a c e , i n e v a l u a t i n g t h e EMU and man's c a p a b i l i t i e s i n t h e l u n a r environment and i n documenting t h e sample c o l l e c t i o n s . The TV w i l l b e u s e f u l i n p r o v i d i n g continuous o b s e r v a t i o n f o r time c o r r e l a t i o n of crew a c t i v i t y w i t h t e l e m e t e r e d d a t a , v o i c e comments, and photographic coverage. �TV r e c e p t i o n , w i t h o u t a d e g r a d a t i o n of b o t h v o i c e and t e l e metered i n f o r m a t i o n , may b e dependent on having t h e LM s t e e r a b l e S-band antenna r a d i a t e t o a 210-foot antenna, e i t h e r t h e Goldstone ( C a l i f o r n i a ) o r t h e Parkes ( A u s t r a l i a ) antenna, o r deploy t h e S-band e r e c t a b l e antenna on t h e l u n a r s u r f a c e . (A comparison of t h e performance expected w i t h t h e 210-foot/ s t e e r a b l e antennas o r 8 5 - f o o t / e r e c t a b l e antennas i s p r e s e n t e d i n T a b l e 3-1 on t h e f o l l o w i n g page.) The e r e c t a b l e antenna makes i t p o s s i b l e t o r e c e i v e TV t r a n s m i s s i o n s w i t h t h e 85-foot antenna d i s h e s a t e i t h e r Goldstone, Madrid, o r Canberra, which a r e e q u i v a l e n t t o t h e 2 1 0 - f o o t / s t e e r a b l e combination. I f a 210-foot antenna i s n o t i n view o r t h e e r e c t a b l e antenna has n o t been deployed, TV coverage may b e o b t a i n e d by a c c e p t i n g t h e l o s s ' o r d e g r a d a t i o n of v o i c e a n d t e l e m e t r y . The f i n a l d e c i s i o n f o r such coverage w i l l b e made i n r e a l t i m e and based on t h e q u a l i t y of t h e communications up t o . . that point. . . ' .:. - For t h e nominal mission, w i t h a J u l y 16 launch d a t e , t h e Goldstone and/or t h e Parkes antennas w i l l b e i n v i e w ' d u r i n g t h e EVA. The coverage provided by t h e 210-foot and 85-foot antennas d u r i n g t h e l u n a r s t a y i s shown i n ~ i g u r e . 3 - 2 . The TV camera w i l l have two primary p o s i t i o n s ' o r f i e l d s of view . f o r coverage of t h e s u r f a c e ' a c t i v i t y . The camera w i l l b e mounted i n ' t h e descent s t a g e Modularized Equipment Stowage Assembly (MESA) t o view ' t h e crewmen's d e s c e n t t o t h e s u r f a c e and t h e CDR's ' a c t i v i t y i n t h e immediate l a d d e r a r e a . (See Figure 3-3). A f t e r t h e LMP'S descent t o ' t h e s u r f a c e , t h e CDR removes t h e camera and t r i p o d from t h e MESA and p l a c e s t h e t r i p o d w i t h camera on t h e s u r f a c e i n an optimum p o s i t i o n ' f o r coverage of subsequent s u r f a c e a c t i v i t y . (See F i g u r e 3-4). �TABLE 3-1 (EM .Mode -~ i Power) ~ h 210 '. MARS STAT1ON 85' MSFN STATION NOMINAL WORST CASE NOMINAL WORST CASE +15.4 +25.4 +23.4 + 7.2 + 1.8 +17.2 +15.2 +11.8 + 9.8 + 7.7 +17.7. E r e c t a b l e Antenna + 8.8 + 9.2, 51.2 kbps Telemetry*" . . EVA Voice (dual) dB EVA EKG & PLSS Data (dual) +.3.8 . . + 9.7 . . T e l e v i s i o n (B&W) . 1.6 kbps Telemetry** +17.4 EVA Voice (dual) + 9.2 + 3.8 + 9.7 EVA EKG & PLSS Data . (dual) ~ e l e v ii so n (B&w) ' S t e e r a b l e Antenna . . . . 51.2 kbps Telemetry** .' EVA Voice (dual) EVA EKG & PLSS Data (dual) + 0.7 - + 1.1 - 4.3 - 1.1 - 6.5 - 0.6 +7.1 EVA Voice (dual) EVA EKG & PLSS Data (dual) - .4.3 - 6.5 T e l e v i s i o n (B&W) + 1.6 - 0.6 1.6 kbps' Telemetry** . . +17.3 + 3.7 + 9.6 +'6.5 + 6.9 . + 1.5 + 7.4 ' +15.1 + 1.5 + 7.4 ' . Based on measured LM-5 'data and MSC t e s t . d a t a on new. (1969) Motorola FM demodulator. The MSC t e s t s were conducted i n t h e ISD E l e c t r o n i c Systems T e s t F a c i l i t y (on one u n i t ) . ' ** + 8.7 + 9.1 + 3.7 + 9.6 1.5 + 1.6 + 9.3 + 1.1 T e l e v i s i o n . (B&W) * +15.7 . For a BER bf . . 16 ' �-16 . 0 .20 J U I 20 ~ 4 8 12 J U ~ Y21 16 20 Greenwich mean time, G a t .~ . . hr. : Figure 3-2.'- Radar coverage during lunar stay f o r launch date of July 16. 0 4 JU~Y 22 �"Z" - plane - / ~ i e wnormal cenl:er line Figure 3-3. - TV field of view from MESA. 18 �Figure 3-4 .-TV field of view from tripod (with Lunar day lens) 18a �3.2.4 S-Band E r e c t a b l e Antenna Deployment ( A l t e r n a t e Timeline) The S-band e r e c t a b l e antenna w i l l be deployed t o i n c r e a s e t h e communications c a p a b i l i t y . I t ' s major impact t o t h e EVA i s i n o b t a i n i n g an e q u i v a l e n t communications c a p a b i l i t y t h a t w i l l b e p o s s i b l e otherwise only i f a 210-foot antenna i s i n view. This communications c a p a b i l i t y may be r e q u i r e d f o r simultaneous TV, v o i c e , and t e l e m e t e r e d d a t a r e t u r n . (See t h e d i s c u s s i o n on t h i s s u b j e c t i n t h e previous s e c t i o n on TV coverage, S e c t i o n 3.2.3). ' . ,, . 3.2.5 The deployment of t h e e r e c t a b l e antenna i s a time-consuming task--deployment time i s expected t o be 19 minutes. However, t h e TV c o v e r a g e , ' w i t h o u t a d e g r a d a t i o n of v o i c e and t e l e m e t r y , gained through t h e use of t h e antenna may r e q u i r e i t t o be deployed. I n t h i s s i t u a t i o n , although i t i s d e s i r a b l e t o a t t a i n t h i s advantage provided by t h e antenna and t o p e r m i t t h e crewman i n s i d e t h e LM t o switch t o t h e e r e c t a b l e antenna e a r l i e r i n t h e t i m e l i n e , t h e crewman's f a m i l i a r i z a t i o n w i t h l u n a r o p e r a t i o n s b e f o r e t h i s p o i n t i s considered t o b e i n s u f f i c i e n t t o s a f e l y and e f f e c t i v e l y accomplish the' deployment task. Photography photography, s t i l l c o l o r photographs w i t h t h e 70mm EL d a t a camera, close-up s t e r e o photographs w i t h t h e Apollo Lunar S u r f a c e Close-up Camera (ALSCC), and motion p i c t u r e s w i t h t h e 16mm ( d a t a a c q u i s i t i o n ) camera, w i l l be a v i t a l p a r t of t h e d a t a c o l l e c t i o n p r o c e s s f o r t h e EVA. A 70mm camera, w i t h b l a c k and w h i t e f i l m , w i l l b e used f o r ' s u r f a c e photography from t h e LM and w i l l b e t r a n s f e r r e d t o ' t h e s u r f a c e . . i f a m a l f u c t i o n of t h e o t h e r camera occurs. . . The crewmen w i l l u s e t h e EL d a t a camera e x t e n s i v e l y on t h e s u r f a c e t o document each major t a s k which they accompl i s h . A d d i t i o n a l photography, such a s panoramas and s c i e n t i f i c documentation, w i l l supplement o t h e r d a t a i n t h e p o s t f l i g h t a n a l y s i s of t h e l u n a r environment and t h e a s t r o n a u t ' s c a p a b i l i t i e s o r l i m i t a t i o n s on conducting l u n a r s u r f a c e o p e r a t i o n s . With t h e ALSCC t h e crewmen may photograph a r e a s of , t h e l u n a r surface not disturbed during t h e landing o r surface a c t i v i t y , t h e i r f o o t p r i n t s , a r e a s a f f e c t e d by t h e LM footpads and t h e s c i e n t i f i c equipment, and o t h e r phenomena of o p e r a t i o n a l and' scientific interest. �The sequence camera, from t h e LM a s c e n t s t a g e window, w i l l p r o v i d e almost continuous coverage of t h e s u r f a c e a c t i v i t y . The Lunar Module P i l o t , who remains i n s i d e t h e a s c e n t s t a g e f o r t h e f i r s t few minutes of t h e EVA, w i l l u s e t h e seauence camera t o document t h e Commander's i n i t i a l s u r f a c e a c t i v i t i e s . Then, b e f o r e h e e g r e s s e s , t h e LMP w i l l p o s i t i o n t h e camera f o r optimum s u r f a c e coverage w h i l e b o t h crewmen a r e on t h e s u r f a c e . And, a f t e r t h e LMP i n g r e s s e s , h e can u s e t h e sequence camera t o p r o v i d e coverage of t h e remaining s u r f a c e activity. A complete d e s c r i p t i o n of t h e camera equipment and t h e i r operat i o n a l procedures, a s w e l l as t h e d e t a i l s of t h e documentation provided by t h e t h r e e cameras, a r e contained i n Reference 6 . 3.2.6 EVA and Environment Evaluation The primary purpose of t h e Environmental F a m i l i a r i z a t i o n p e r i o d , e a r l y i n t h e t i m e l i n e , i s t o allow t h e crew s u f f i c i e n t time t o adapt t o t h e new environment and o p e r a t i n g c o n d i t i o n s . The EVA and Environment E v a l u a t i o n , however, i n v o l v e s a d e t a i l e d i n v e s t i g a t i o n and documentation of a crewman's c a p a b i l i t y w i t h i n t h e c o n s t r a i n t s of t h e EMU, t h e PLSSIEMU performance under v a r y i n g c o n d i t i o n s of s u n l i g h t , shadow, crewman a c t i v i t y o r i n a c t i v i t y , and t h e c h a r a c t e r i s t i c s of t h e l u n a r environment which i n f l u e n c e o p e r a t i o n s on t h e s u r f a c e . The p r e l i m i n a r y f a m i l i a r i z a t i o n w i l l be of t h e most b e n e f i t i n r e a l time--to p r e p a r e t h e crewmen t o o p e r a t e d u r i n g t h i s EVA. On t h e o t h e r hand, t h e EVA and Environment E v a l u a t i o n p e r i o d should b e of s i g n i f i c a n t v a l u e f o r f u t u r e l u n a r s u r f a c e e x p l o r a t i o n . From t h e assessment of d a t a g a t h e r e d d u r i n g t h i s p e r i o d , s u f f i c i e n t knowledge should b e gained t o acc u r a t e l y p r e d i c t t h e c a p a b i l i t i e s and l i m i t a t i o n s of t h e a s t r o n a u t and h i s equipment f o r f u t u r e l u n a r s u r f a c e e x t r a vehicular activity. During t h e EVA and Environment E v a l u a t i o n t h e LMF w i l l determine, i n d e t a i l , t h e combined e f f e c t s of t h e EMU c o n s t r a i n t s and l u n a r g r a v i t y on h i s p h y s i c a l c a p a b i l i t i e s . H e w i l l compare h i s c a p a b i l i t i e s i n t h i s l u n a r environment w i t h s i m i l a r experiences d u r i n g e a r t h g r a v i t y and s i m u l a t e d l u n a r g r a v i t y e x e r c i s e s . He w i l l observe how t h e l u n a r s u r f a c e i s a f f e c t e d by t h e a c t i o n s he performs and c a r e f u l l y examine . t h e t e r r a i n t o determine t h e s u r f a c e c h a r a c t e r i s t i c s . Also, h e w i l l determine h i s v i s u a l p e r c e p t i o n of t h e s u r f a c e f e a t u r e s and h i s v i s u a l a c u i t y w i t h i n t h e c o n s t r a i n t s of t h e e x t r a v e h i c u l a r v i s o r assembly (EWA). �3.2.7 Sample Collections The nominal plan is to conduct three sample collections of lunar surface material. They are, in order of priority, the contingency, the bulk, and the documented sample collections. The contingency sample collection is a simple task which can be accomplished within a few minutes early in the EVA timeline. This will assure the'return of a small sample in a contingency situation where a crewman may remain on the surface for only a short period of time. One to two kilograms .of loose material will be collected near the LM ladder and the sample bag restowed in the suit pocket to be carried into the ascent stage when the crewman ingresses. In the bulk sample collection at least 10 kilograms of unsorted surface debris and selected rock chunks'willbe placed in a special container, an Apollo Lunar Sample Return Container (sRC), to provide a near vacuum environment for its Apollo return to the Lunar Receiving Laboratory (LRL). Lunar Handtools (ALHT), stowed in the MESA with the SRC, will be used to collect this large sample (30 to 60 pounds) of loose lunar material from the surface near the MESA in Quad IV of the LM. As each rock sample or scoop of loose material is collected it will be placed into a large sample bag. Placing the sealed bag, rather than the loose material directly into the SRC, also prevents contamination and possible damage to the container seals. The documented sample collection, like that of the bulk sample collection, will involve a large mass of lunar material placed into an SRC for return to earth: However, the documented sample will differ significantly in content and in its collection process. As the name implies the documented sample collection will involve the documentation of the individual samples and the area from which they are taken. It can be classified as a very limited lunar field geology investigation. �Within t h e documented sample c o l l e c t i o n a core t u b e sample i s f i r s t c o l l e c t e d t o p r o v i d e an a s e p t i c and s t r a t i f i e d sample n e a r t h e LM. A t a s i t e r e p r e s e n t a t i v e o f . t h e l a n d i n g a r e a , t h e crew w i l l examine, d e s c r i b e , photograph, and c o l l e c t rock fragments and l o o s e s u r f a c e m a t e r i a l samples and p l a c e them i n d i v i d u a l l y i n pre-numbered bags. ' T h e samples, i n t h e s m a l l bags numbered one through f o u r t e e n , a r e placed i n a l a r g e bag f o r t r a n s f e r t o and stowage i n t h e documented sample SRC. I f time p e r m i t s a f t e r c o l l e c t i n g t h e s m a l l bags of samples, t h e crew w i l l c o l l e c t two environment samples, r e p r e s e n t a t i v e of t h e b u l k sample, and a second c o r e t u b e sample. Additiona l l y , t h e l a r g e sample bag w i l l be f i l l e d , a s t h e b u l k sample bag, t o r e t u r n t h e maximum amount of s u r f a c e m a t e r i a l . The v a r i o u s samples w i t h i n t h e documented sample c o l l e c t i o n w i l l b e t a k e n from a r e a s n e a r t h e LM o u t t o p o s s i b l y 300 f e e t away. Although t h e l i m i t i n g d i s t a n c e from t h e LM f o r t h i s f i r s t s u r f a c e mission i s 300 f e e t , t h e r e a r e s e v e r a l reasons f o r t h e crew t o remain w i t h i n 100 f e e t . F i r s t , s i n c e t h e documented sample c o l l e c t i o n w i l l b e l a t e i n t h e EVA, t h e c a p a b i l i t y of t h e crew and t h e i r equipment w i l l b e l i m i t e d a t t h i s time. A d d i t i o n a l l y , on t h i s f i r s t l a n d i n g mission a r e l a t i v e l y cons e r v a t i v e approach i s necessary. Also, i t i s u n l i k e l y t h a t t h e t e r r a i n a t 300 f e e t w i l l be s i g n i f i c a n t l y d i f f e r e n t from t h e t e r r a i n w i t h i n 100 f e e t of t h e LM. 3.2.8 Lunar Module I n s p e c t i o n The purpose of t h e LM i n s p e c t i o n i s t o v i s u a l l y check and p h o t o g r a p h i c a l l y document t h e e x t e r n a l c o n d i t i o n of t h e LM a f t e r t h e f l i g h t t o t h e l u n a r s u r f a c e and t h e e f f e c t s of t h e LM l a n d i n g on t h e l u n a r s u r f a c e . The i n s p e c t i o n d a t a w i l l b e used t o v e r i f y t h e LM a s a s a f e and e f f e c t i v e v e h i c l e f o r l u n a r e x c u r s i o n s . The d a t a w i l l a l s o b e used t o g a i n more knowledge of t h e l u n a r s u r f a c e c h a r a c t e r i s t i c s . I n g e n e r a l ' t h e b e n e f i t of t h e . i n s p e c t i o n w i l l s e r v e t o advance t h e equipment d e s i g n and our understanding of t h e environment i n which i t operates. The crewmen w i l l methodically i n s p e c t and r e p o r t t h e s t a t u s of a l l e x t e r n a l p a r t s and s u r f a c e s of t h e LM which a r e v i s i b l e t o them. They w i l l examine t h e l u n a r s u r f a c e about t h e LM t o determine t h e i n t e r a c t i o n s of t h e LM footpads w i t h t h e l u n a r s o i l f o r s t u d y of t h e l u n a r s u r f a c e p r o p e r t i e s . The s t i l l c o l o r �photographs w i t h t h e Hasselblad and closeup cameras, w i l l supplement t h e i r v i s u a l documentation f o r p o s t f l i g h t engineeri n g a n a l y s i s and d e s i g n v e r i f i c a t i o n . They w i l l observe and photograph t h e Reaction C o n t r o l System (RCS) e f f e c t s on t h e LM, t h e l a n d i n g g e a r performance, t h e i n t e r a c t i o n s of t h e s u r f a c e and f o o t p a d s , and t h e Descent P r o p u l s i o n System (DPS) e f f e c t s on t h e s u r f a c e a s w e l l a s t h e g e n e r a l c o n d i t i o n of a l l . quadrants and l a n d i n g s t r u t s . (Refer t o F i g u r e s 3-5, 3 - 6 , 3-7, and 3-8 f o r t h e major LM i n s p e c t i o n p o i n t s .) 3.2.9 Experiment Deployments . . There a r e t h r e e s c i e n t i f i c experiments which w i l l ' b e deployed. The S o l a r Wind composition (SWC) experiment deployment, although of lowest p r i o r i t y , i s accomplished f i r s t a s i t is a s i m p l e t a s k and t h e r e s u l t s depend on t h e exposure time. A t l e a s t a n hour of exposure time i s d e s i r e d b e f o r e i t is p l a c e d i n a n SRC f o r r e t u r n t o e a r t h . The o t h e r two experiments, t h e P a s s i v e Seismic (PSE) and L a s e r Ranging R e t r o - r e f l e c t o r (LR3), a r e deployed l a t e r b u t w i l l c o n t i n u e t o r e t u r n d a t a a f t e r t h e mission. The SWC c o n s i s t s of a p a n e l of very t h i n aluminum f o i l r o l l e d and assembled i n t o a combination h a n d l i n g and deployment c o n t a i n e r . It i s stowed i n t h e MESA. Once t h e thermal b l a n k e t i s removed from around t h e ~ S equipment A i t is a s i m p l e t a s k t o remove t h e SWC, deploy t h e s t a f f and t h e f o i l "window shade", and p l a c e i t i n d i r e c t s u n l i g h t where t h e f o i l w i l l b e exposed t o t h e s u n ' s r a y s . The SWC i s designed t o e n t r a p n o b l e gas c o n s t i t u e n t s of t h e s o l a r wind, s u c h ' a s Helium, Neon, Argon, Krypton and Xenon. The f o i l is . l a t e r r o l l e d up, removed from t h e s t a f f , and placed i n an SRC. I f i t i s known a t t h e time t h e b u l k sample SRC i s packed t h a t a documented sample w i l l n o t b e c o l l e c t e d , t h e SWC w i l l b e p l a c e d i n t h e b u l k sample SRC. I f t h e b u l k sample SRC h a s been s e a l e d b e f o r e d e c i d i n g n o t t o c o l l e c t t h e documented sample t h e SWC may b e p u t i n t o t h e LMP's s u i t pocket f o r t r a n s f e r t o t h e a s c e n t s t a g e . A t t h e same t i m e t h e f o i l i s recovered, t h e a s t o n a u t w i l l push t h e s t a f f i n t o t h e l u n a r s u r f a c e t o determine, f o r p o s t f l i g h t s o i l mechanics a n a l y s i s , t h e depth of p e n e t r a t i o n . �Pad and surface descent stage Figure 3-5. - Quad I inspection points. Figure 3-6. - Quad II inspection points. 24 �S-band steerable antenna :ation Oxidizer pressurization Figure 3-7. - Quad III inspection points. S-band DPS effects on surface Figure 3-8. . - Quad I37 inspection points. �The PSE, o r t h e PSE package (PSEP), is one of two packages of t h e E a r l y Apollo S c i e n t i f i c Experiments Package (EASEP). It w i l l b e p l a c e d on t h e l u n a r s u r f a c e t o monitor l u n a r seismic a c t i v i t y and d e t e c t meteriod impacts, f r e e o s c i l l a t i o n s of t h e moon, and l u n a r i n t e r n a l a c t i v i t y . It may a l s o d e t e c t s u r f a c e deformations and v a r i a t i o n s of e x t e r n a l g r a v i t a t i o n a l f i e l d s a c t i n g on t h e moon. Data from t h i s s e l f c o n t a i n e d , solar-powered experiment package s h o u l d r e v e a l t h e p r o p e r t i e s of t h e s e i s m i c e v e n t s , t h e p h y s i c a l p r o p e r t i e s of t h e s u b s u r f a c e m a t e r i a l s , and t h e g e n e r a l s t r u c t u r e of t h e lunar interior. The LR3 i s a l s o one of t h e two EASEP packages. The package p r o v i d e s a c o r n e r r e f l e c t o r ( a c t u a l l y a n a r r a y of 100 r e f l e c t o r s ) f o r l a s e r ranging from e a r t h . From t h i s experiment t h e n a t u r e of t h e e a r t h ' s i r r e g u l a r r o t a t i o n may b e determined. Also, t h e d a t a w i l l h e l p r e f i n e t h e l u n a r motions and t h e r e l a t i v e motion of t h e e a r t h and moon. The PSEP and LR3 a r e on s e p a r a t e p a l l e t s which a r e stowed i n ' t h e S c i e n t i f i c Experiment (SEQ) bay of t h e d e s c e n t s t a g e Quad 11. I n t h e nominal deployment t h e LMP removes b o t h packages and c a r r i e s them t o t h e deployment s i t e simultaneously. 15 degrees The,crewmen w i l l s e l e c t a l e v e l s i t e , nominally w i t h i n of t h e LM -Y a x i s and 70 t o 110 f e e t from t h e LM. The s e l e c t i o n of t h e s i t e i s based on a compromise between a s i t e which minimizes t h e e f f e c t s of t h e LM a s c e n t e n g i n e d u r i n g l i f t o f f h e a t and contamination by d u s t and i n s u l a t i o n d e b r i s (kapton) from t h e LM d e s c e n t s t a g e , and a convenient s i t e n e a r t h e SEQ bay. + 3.2.10 U s e of t h e Lunar Equipment Conveyor The Lunar Equipment Conveyor (LEC) i s a d e v i c e which t h e a s t r o n a u t s w i l l u s e d u r i n g t h e EVA t o t r a n s f e r equipment t o o r from t h e a s c e n t s t a g e . It may a l s o b e used by t h e crewmen a s a s a f e t y t e t h e r when moving down t h e l a d d e r o r as a n a i d i n ascending t o t h e a s c e n t s t a g e . The LEC is a t h i n 60 fo-ot continuous loop of one i n c h wide s t r a p , which loops through a s u p p o r t p o i n t i n t h e a s c e n t s t a g e and back t o t h e crewman on t h e s u r f a c e . The end of t h e loop i s c l o s e d by two hooks, a t t a c h e d t o g e t h e r , which �p r o v i d e a means of s e c u r i n g equipment t o t h e LEC f o r t r a n s f e r . The crewman on t h e s u r f a c e can e f f e c t a t r a n s f e r t o t h e a s c e n t s t a g e by p u l l i n g t h e top s t r a p which causes equipment hooked t o t h e lower s t r a p t o move i n t o t h e a s c e n t stage. Although t h e t r a n s f e r of equipment with t h e LEC i s simple i n p r i n c i p l e , t h e a c t u a l t r a n s f e r o p e r a t i o n can r e q u i r e a s i g n i f i more i f c a u t i o n i s . n o t obc a n t amount of time and e f f o r t s e r v e d i n keeping t h e s t r a p s untangled o r i f t h e p r o p e r o p e r a t i o n a l procedures a r e n o t used. Because of t h e time involved (up t o f i v e minutes p l u s a r e s t p e r i o d ) , t h e number of equipment t r a n s f e r s i s k e p t t o a minimum. I n t h e nominal t i m e l i n e t h r e e t r a n s f e r s a r e planned, one t o t r a n s f e r t h e Hasselblad camera t o t h e s u r f a c e and one t r a n s f e r f o r each of t h e two SRC's. - EVA Termination For EVA t e r m i n a t i o n t h e r e a r e s e v e r a l advantages gained by one crewman i n g r e s s i n g b e f o r e an SRC i s t r a n s f e r r e d . ~ l t h o u g h i t i s p o s s i b l e t o t r a n s f e r an SRC i n t o t h e a s c e n t s t a g e b e f o r e t h e f i r s t crewman i n g r e s s e s , t h e crewman i n s i d e w i l l p r o v i d e some a s s i s t a n c e d u r i n g t h e t r a n s f e r . A d d i t i o n a l l y , h e w i l l remove t h e SRC and p l a c e i t where i t does n o t i n t e r f e r e w i t h i n g r e s s . The f i r s t crewman t o i n g r e s s w i l l a l s o make a LM system check, change t h e sequence camera f i l m magazine, and r e p o s i t i o n t h e camera t o cover t h e SRC t r a n s f e r and o t h e r crewman's l a d d e r a s c e n t . A s each man b e g i n s h i s EVA t e r m i n a t i o n h e w i l l c l e a n t h e EMU. Although t h e crew w i l l have a very l i m i t e d c a p a b i l i t y t o remove l u n a r m a t e r i a l from t h e i r EMU'S, they w i l l a t t e m p t t o brush o f f any d u s t o r p a r t i c l e s from t h e p o r t i o n s of t h e s u i t which they can reach and from t h e b o o t s on t h e footpad and l a d d e r . I n t h e EVA t e r m i n a t i o n t h e r e a r e two t a s k s which w i l l r e q u i r e some i n c r e a s e d e f f o r t . The f i r s t i s t h e a s c e n t from t h e . footpad t o t h e lowest l a d d e r rung. I n t h e unstroked p o s i t i o n t h e v e r t i c a l d i s t a n c e from t h e top of t h e footpad t o t h e lowest l a d d e r rung i s 31 i n c h e s . I n a nominal l e v e l l a n d i n g t h i s d i s t a n c e w i l l be decreased only about f o u r i n c h e s . Thus, u n l e s s t h e s t r u t i s s t r o k e d s i g n i f i c a n t l y t h e crewmen a r e r e q u i r e d t o s p r i n g up u s i n g t h e i r l e g s and arms t o b e s t advantage t o r e a c h t h e bottom rung of t h e l a d d e r from t h e footpad. �The second t a s k w i l l be t h e i n g r e s s o r t h e crewmen's movement through t h e h a t c h opening t o a s t a n d i n g p o s i t i o n i n s i d e t h e LM. The h a t c h opening and t h e space i n s i d e t h e LM a r e small. T h e r e f o r e , t h e crewmen must move slowly t o p r e v e n t p o s s i b l e damage t o t h e i r EMU'S o r t o t h e exposed LM equipment. Before t h e crew c l o s e s t h e h a t c h and b e g i n s t h e c a b i n r e p r e s s u r i z a t i o n , they w i l l j e t t i s o n t h e equipment they no l o n g e r need. The i t e m s t o j e t t i s o n a r e t h e used ECS c a n n i s t e r and b r a c k e t , OPS b r a c k e t s ( a d a p t e r s ) , and 3 a r m r e s t s . Numerous p i e c e s of l o o s e equipment w i l l b e l e f t on t h e l u n a r s u r f a c e a f t e r they have been deployed o r used d u r i n g t h e EVA. A complete l i s t of t h i s equipment except f o r a few pip-pins, b r a c k e t s , and o t h e r s m a l l p i e c e s of t h e l a r g e r p i e c e s of equipment l i s t e d , i s p r e s e n t e d a s Table 3-2 on t h e f o l l o w i n g page �TABLE 3-2 Loose Equipment L e f t on Lunar S u r f a c e During EVA . TV Equipment . . .. .. camera tripod h a n d l e l c a b l e assembly MESA b r a c k e t . S o l a r Wind Composition s t a f f Apollo Lunar Handtools scoop tongs e x t e n s i o n handle hammer gnomon Equipment stowed i n sample r e t u r n c o n t a i n e r s (outbound ) e x t r a York mesh packing m a t e r i a l SWC bag ( e x t r a ) spring scale unused s m a l l sample bags two c o r e tube b i t s two SRC s e a l p r o t e c t o r s environmental sample c o n t a i n e r s 0 r i n g s and s m a l l r o d s i n l i d s .. . .. . . . . .. - - . . . Apollo Lunar S u r f a c e Close-up Camera . EL Data Camera (magazine r e t u r n e d ) (film c a s s e t t e returned) EVA t e r m i n a t i o n Lunar Equipment Conveyor ECS c a n n i s t e r and b r a c k e t OPS b r a c k e t s Three a r m r e s t s Bag of used u r i n e bags . . . . . Post-EVA equipment j e t t i s o n Two P o r t a b l e L i f e Support Systems L e f t Hand S i d e Stowage Compartment (with equipment i n s i d e ) One a r m r e s t . . . �3.3 SUMMARY TIMELINE NOMINAL LUNAR SURFACE EVA n LEGEND I HCC.H ~YL:LRV." :: i.. I I ACIlVIIV ...'..., .. .~C.OV..l b0t~.0. 1.10 1:20 1439 \Irnt\<I it: is 1.40 *.:....z... .................................................... o u t COUY 5 m m . ru ~ m w t c r d o ~ p s s c c r ol.0 ~v OO(,YCITCO MCST/PMO~O IAYPLC :JUIC:,~S ius .Tact C L O I ~ . C DD . C I O I I < .OIDLO' L*' .Rat0 b C10SC.u. m .on* - .(a JcsLo."c:. 8.r ."CYWC I I ,.W.l"l*'S lOrYI [.,I> I 1XMIIVI.l am ! 0. T o o 1 C"M.l"I.lS 4- DO(.YI.113 ( A Y 4 1 C*L.L-"M .u~wt I);%* sw T O \ v 4 . ' v. ... c-*I .C,OSC S I P 6." I ~IILCCI < OWI OC.LO~YC.I .C.*.v 1.20 1.30 k ... $811 m s s * v c $cn\unr KC CL0SC.C. 1.10 I ..r I S ~ C t I P 1J 0 1 4 0 ' .OCPIO, I ur ~aeaa*~.. hi'\'\ -. --. -- -- 1:10.-. ��3.4 NOMINAL TIMELINE. LUNAR SURFACE EVA LMP - CD R - o+oo mm m a C r m ,m z m 0 mm z 00 D - oz x m - + I == C NOTE : DETAILED PROCEDURES ARE PRESENTED I N " F I N A L EVA PROCEDURES APOLLO 11" SUBMITTED BY EVA BRANCH, FC -zs 7JC <3 m - -I= W-I -I- TURN TV ON START SEQUENCE CAMERA (SC) I ' .I IPLAY UliT LEC I DESCEND TO FOOTPAD CHECK ASCENT PROCEDURES I z 3 r u I H O Z Z CHANGE SC FR TO 24/SEC STEP TO SURFACt RESTICHECK E14U I I I - .-ISTOW LEC - ~ - 0+10 - MONITOR CDR A C T I V I T Y PLAY OUT LEC MOVE TO'POSITION AND RELEASE MESA w cnD -m LMP - DEPRESS CABIN FROM 3.5 P S I OPEN HATCH INSURE SUBLIMATOR ICED PERFORM F I N A L SYSTEMS CHECKS CONFIRM "GO" FOR EVA - Wcn 0 CDR - II M O V E 1'HROUGH HATCH CHECK INGRFSS PROCEDURE I 11 1 APOLLO EDITION FINAL t 1 CHECK AND DISCUSS BALANCEISTABILITY I I 1 TO 121SEC VISUALLY MONIT~R CDR ACTIVITY PROVIDE CHECKLIST ASSISTANCE I + ASSIS CDR PLAY OUT LEC CHANGE SC F I L M MAG CHANGE FR TO 61SEC /-L MISSION CHANGE SC% - DATE JUNE 27, 1 9 6 9 rC/ I MISSION TIME I DAY1am I PAGE 1 �NOMINAL TIMELINE CDR - LMP - LMP - CDR - II I- REST/CHECK EMU CHECK LM AND EMU STA* sc 1 t UNSTOW CSC AllD DEPLOY HANDLE MONITOR AN; EXTEND BAG COLLECT SAMPLE + PHOTO EGRESS I DETACH BAG AND DISCARD HANDLE -I- I STOW SAMPLE I MONITOR TRANSFER STILL CAMERA TO SURFACE PREPARE FOR CAMERA TRANSFER ASSIST CDR PERFORM COMM CHECK AND PHOTO LMP C I REMOVE TRIPOD I PERF OR^ FI~AL LM AND EMU CHECK CONFIRM "GO" FOR EVA PLACE SPARE CAMERA ON LM FLOOR I MISSION APOLLO 1 1 I I FINAL I 1 JUNE t tI t DET'ERMI NE WALKING CAPABILITY REMOVE TV CABLE 1 I -I- REMOVE CAMERA CARRY TV TO DEPLOY S I T E L 1 EDITION f' \D LENS WA TO I t CHECK ERWIN AND LIGHTING STEP TO SURFACE REST/CHECK EMU + CHANGE FROM I CHECK AND REPORT LM STATUS DESCEND TO PAD CHECK ASCENT PROCEDURE C ECK BALANCE/STABILITY REACH CAPABILITY TETHER' CAMERA t I- I t PREPARE MESA FOR TV DEPLOYMENT REST/CHECK EMU MOVE TH'RU HATCH CHECK INGRESS PROCEDURE DATE 27. 1 9 6 9 MISSION TIME 112+54 - 113+18 I 1 DAY/ REV 5/20 I PAG€ 2 of 7 1 �NOMiNAL TIMELINE CDR - LMP - . II CDR - LMP - �NOMINAL TIMELINE LMP - CDR - ?' + CARRY ALSCC REPORT STATUS QUAD I V REPORT STATUS AND PHOTO -Y GEAR REMOVE PACKAGE 1 (PSE) PHOTO QUAD I V TAKE PHOTO PANORAMA + REMOVE PACKAGE 2 ( L R ~ ) I I PHOTO >Y GEAR 1 , PHOTO EASEP OFFLOAD TAKE CLOSE-UP PHOTOS TAKE CLOSE-UP PHOTOS QUAD. I11 + t 4- TRANSFER CAMERA TO CDR 1 OPEN SEQ BAY DOOR C I , PHOTO E A S E OFF LOAD MISSION APOLLO 11 I 1 EDITION FHVAL I 1 i t T RESTICHECK EMU C DEPLOY PSE $- DEPLOY L R ~ -IREPORT STATUS AND PHOTO QUAD I 1 t CLOSE SEQ BAY DOOR RESTISELECT DEPLOY S I T E CARRY CAMERAS TO CARRY EASEP DEPLOY S I T E PACKAGES REPORT POSITION TO DEPLOY S I T E FROM LM PHOTO -Z GEAR TETHER S T I L L CAMERA t T_L PHOTO qUAD I11 REPORT STATUS -Z GEAR 7' -1- REMOVE ALSCC FROM MESA AND DEPLOY 1 REPORT STATUS +Y GEAR 1 LMP - CDR - II I PHOTO L R ~ MOVE DATE JUNE 13, 1969 MISSION TIME 113+42 - 114+06 I % PSE T I 1 TAKE CLOSE-UP PHOTOS DAY/ REV 5/20 I PAGE 4 of 7 ��NOMINAL TIMELIN E CDR - LMP - CDR - LMP - T PLATFORM t RESTIPHOTO LMP 1 t REMOVE ALSCC F I L M STOW I N CSC POCKET STOW ALSCC F I L M I -L- t MOVE TO MESA PLACE SCOOP BY MESA MOVE TO MESA PLACE SAMPLE BAG ON SCALE t OPEN L A ~ G EENVIR. SAMPLE CONTAINER. COLLECT LOPSE MATERIAL -L + RETRIEVE SWC t HOLD CONTAINER SEAL AND STOW t SCOOP LOOSE + PACK SRC I F T I M E AVAILABLE COLLECT CORE SAMPLE CLOSE AND SEAL SRC MOVE TO LADDER CLEAN EMU t 1, APOLLO ASSIST CDR, + + HOLD S ~ CBAG 1. 11 1 T TRANSFER BULK SAMPLE SRC AND CAMERA MAG. MATERIAL INTO SAMPLE BAG PLACE SWC I N BAG MISSION CHANGE sc F I L M REORIENT CAMERA CHANGE FR TO 6/SEC I I PUSH STAFF INTO SURFACE. ASSESS FORCE PHOTO r REMOVE CAMERA MAGAZINE AND CONNECT TO LEC OPEN SMALL CONTAINER COLLECT ROCK SAMPLE HOLD CONTAINER SEAL AND STOW + INGRESS DISCONNECT AND STOW SRC AND CAMERA MAG. I I EDIVION. FINAL I DATE IJUNE 1 9 6~9 ~ , . MISSION TIME 114+30 - 114+54 1 DAY/ REV 5/20-21 I t PAW 6 of 7 I �NOMINAL TIMELINE CDR - LMP - - T - t1 -. JETTISON EQUIPMENT CLOSE HATCH - Ct STOP SC ' 2+40 LMP - CDR - CABIN REPRESS 1 - - DISCONNECT LEC AND - M I S S I O N TIME FINAL I JUNE 27, 1969 114+54 - 115+f8 I DAY/ REV 5/21 I PAaE 7 of 7 I �SUN I -z 100 FEET OF - FIGURE 3-9. - SCALE 0' PROBABLE AREAS FOR LUNAR SURFACE ACTIVITY 5' 10' �3.5 Detailed Procedures 3.5.1 Nominal Activities Sequence Section Event Final Pre-EVA Operations Page 40 CDR Initial EVA CDR Environmental Familarization Contingency Sample Collection Preliminary Checks LMP Initial EVA . VIII . VII TV Deployment LME' Environmental Familiarization SWC Deployment EVA and Environment Evaluation XI. Bulk Sample Collection LM Inspection* EASEP Deployment XIV . XV. XVI . XVII. * Documented Sample Collection LMP EVA Termination SRC Transfer CDR EVA Termination Nominally, the Apollo Lunar Surface Close-up . . Camera (ALSCC) will be deployed during the LM inspection. �3.5.2 Procedures LMP - CDR I. FINAL PRE-EVA OPEUTIONS NOTE: For t h e d e t a i l e d procedures of t h i s s e c t i o n , r e f e r t o t h e " F i n a l EVA Procedures Apollo ll", which is submitted by t h e EVA Branch, FCSD D e p r e s s u r i z e c a b i n from 3.5 p s i Open h a t c h I n s u r e s u b l i m a t o r iced Perform f i n a l systems checks Confirm "go" f o r EVA CDR INITIAL EVA 11. Move through h a t c h (with LEC t e t h e r e d ) Check i n g r e s s procedure A s s is t CDR ' . Perform communications . check w i t h MSFN - Compare l e v e l , c l a r i t y and r e l a y c a p a b i l i t y w i t h t h a t experienced i n s i d e t h e LM. NOTE: F u r t h e r mention of communications checks w i l l b e made only when communication c o n d i t i o n s change, however, t h e y w i l l b e conducted a s r e q u i r e d f o r system o r crewmen monitoring. Move t o p o s i t i o n on l a d d e r t o r e l e a s e MESA Play o u t LEC and u s e a s s a f e t y t e t h e r .. �CDR - Release MESA(1f MESA does n o t deploy, p u l l manual deployment lanyard l o c a t e d on l e f t s i d e of MESA) NOTE: I f t h e MESA w i l l n o t deploy a f t e r p u l l i n g t h e manual deployment lanyard, t h e following EVA t a s k s cannot b e accomplished: 1) 2) 3) 4) 5) 6) Turn TV on and v e r i f y TV reception . . . S t a r t sequence camera. Check o r i e n t a t i o n and frame r a t e a t 12 frameslsec TV Deployment (no TV coverage) SWC Deployment Bulk Sample C o l l e c t i o n Documented Sample C o l l e c t i o n SRC T r a n s f e r Close-up Photography Descend l a d d e r t o footpad. Checkpad-to-1adder.ascent procedures Play o u t LEC Change sequence camera (SC) frame r a t e (FR) t o 2 4 l s e c Step t o s u r f a c e R e s t b e s i d e ladderlcheck EMU. Check RCU. Report 02 and s u i t p r e s s u r e Change SC FR t o 12Isec. Check LM and EMU. Check RCU and r e p o r t 0 2 and s u i t p r e s s u r e Assess e g r e s s / i n g r e s s c a p a b i l i t y 111. CDR ENVIRONMENTAL FAMILIARIZATION Detach and temporarily stow LEC on gear s t r u t o r ladder I n t h e v i c i n i t y of t h e l a d d e r , check i n d i v i d u a l s t a b i l i t y and perform preliminary m o b i l i t y evaluation Check and r e p o r t b a l a n c e l s t a b i l i t y : a. b. c. - l e a n forward, E f f e c t of CG s h i f t backward, and t o each s i d e Downward reach A m motion e f f e c t s Visually monitor CDR a c t i v i t y . Provide c h e c k l i s t a s s is t a n c e �E v a l u a t e and r e p o r t walking capability: Change SC f i l m magazine when necessary. Change FR t o 61sec a. . B a l a n c e b. B e s t pace c. Boot p e n e t r a t i o n d. T r a c t i o n e. S o i l s c a t t e r i n g (cohesion) f . S o i l adhesion g. General comments . . . . . . ~ e s t l c h e c kEMU. Check RCU. Report 02 and s u i t p r e s s u r e . Report p h y s i c a l comfort. Assess EVA capsbility Check LM and EMU. Check RCU Report 02 and s u i t p r e s s u r e . . IV. . CONTINGENCY SAMPLE COLLECTION Remain w i t h i n a few f e e t of l a d d e r Remove t h e CSC from s u i t pocket Deploy t h e CSC h a n d l e and p u l l s t r a p a t b a s e of bag t o open C o l l e c t sample ( i n undisturbed area) P u l l l o c k i n g p i n on . h a n d l e r e l e a s e lever P r e s s r e l e a s e l e v e r and s e p a r a t e h a n d l e from l i p l b a g assembly Discard handle under o r away from LM Detach bag from l i p assembly Discard l i p assembly under o r away from LM S e a l sample bag Restow and s e c u r e bag i n s u i t pocket S t a r t SC. .Check FR a t 6 / s e c V i s u a l l y monitor CDR a c t i v i t y Reorient SC i f necessary �CDR - LMP V. PRELIMINARY CHECKS T r a n s f e r Hasselblad EL Data camera (with c o l o r f i l m and 60mm l e n s ) t o s u r f a c e : a. Remove LEC from temporary stowage l o c a t i o n Prepare t o t r a n s f e r t h e E l e c t r i c Hasselblad camera t o s u r f a c e b. Walk o u t +Z w i t h LEC P l a y o u t LEC. Remove LEC stowage bag and stow i n LHSSC c. T r a n s f e r camera t o s u r f a c e by p u l l i n g on lower s t r a p of LEC A s s i s t CDR, i f necessary d. Detach camera from LEC and t e t h e r t o s u i t . Mount camera on RCU b r a c k e t when d e s i r e d Change sequence camera FR t o llsec NOTE: Only t h e one Hasselblad camera is t r a n s f e r r e d t o t h e surface. I f a f a i l u r e o c c u r s , manual f i l m advancemand and a f u s e change a r e t h e only a c t i o n s p o s s i b l e t o c o r r e c t t h e malfunction. I f malfunction is not c o r r e c t e d , t h e 70mm Hasselblad, w i t h b l a c k and w h i t e f i l m and 80mm l e n s , can be transferred. e. P l a c e LEC back a t stowage location Check and r e p o r t LM s t a t u s . From immediate v i c i n i t y of t h e l a d d e r , check and r e p o r t : a. S t a b i l i t y of LM ( a l l pads contacting surface, t e r r a i n slope, boulders, c r a t e r s ) R e o r i e n t c'amera t o view CDR activity . (The LMP p r e p a r e s t o e g r e s s ) �CDR - b. Gear s t a t u s ( t a k e two photos, one each of +Y and -Y, and one of +Z p a d l s u r f a c e ) (1) Contact (2) P e n e t r a t i o n , s l i p , b u r i a l (3) S t r o k e . . (4) S o i l adhesion c . ? DPS s k i r t s t a t u s ( 1 photo) d. DPS e f f e c t on s u r f a c e : (1) Crater ' (2) R a d i a l e r o s i o n Perform f i n a l LM and EMU check. Confirm "GO" f o r two-man EVA P l a c e s p a r e Hasselblad camera on f l o o r a t 1 e f t . s i d e of +Z hatch. Check EVA t e t h e r attached (Refer t o t h e n e x t s e c t i o n f o r LMP e g r e s s p r o c e d u r e s ) . Check t e r r a i n s t a t u s f o r crew operations : . . a. Check s l o p e , o b s t r u c t i o n s and roughness i n (1) MESA a r e a (2) TV deployment a r e a (3) S-band antenna deployment area (4) Quad I a r e a b. Check l i g h t i n g l v i s i b i l i t y s t a t u s : (1) B r i g h t and d a r k a r e a s (2) TV deployment (3) MESA (4) S-band antenna a r e a (5) General sampling a r e a s ( t a k e two ( s t e r e o ) photos of b u l k sample and one photo, c l o s e up, of contingency sample a r e a ) (6) Up sun (7) Cross sun (two photos, one each d i r e c t i o n ) (8) Down sun LMP INITIAL EVA Res t/Monitor and photograph LMP e g r e s s and d e s c e n t t o R e o r i e n t SC . . . surface Photo (3) LMP Move through hatch. Check i n g r e s s procedure ( P u l l +Z hatch closed) �CDR - LMP Perform communications check (Include r e l a y check with CSM, i f p o s s i b l e ) Photo (3) LMP Descend l a d d e r t o footpad Check pad-to-ladder procedures Photo (3) LMP ascent Step t o s u r f a c e (Deploy TV, see procedures below) Rest b e s i d e ladderlcheck Assess e g r e s s l i n g r e s s capabilities EMU. VII. TV DEPLOYMENT Walk t o MESA Adjust MESA h e i g h t , i f necessary, by p u l l i n g upward on adjustment strap P u l l s t r a p (velcroed) t o remove MESA thermal b l a n k e t from around TV l e n s Complete removal of thermal blanket Remove t r i p o d from MESA: a. P u l l two s t r a p s t o unsnap b. c. d. e. tripod L i f t t r i p o d from MESA Extend t e l e s c o p i n g s e c t i o n Deploy l e g s P l a c e on s u r f a c e near r i g h t s i d e of MESA Walk t o r i g h t s i d e of MESA Remove wide angle l e n s from TV camera and stow on MESA holder Remove LD l e n s from holder and a t t a c h t o camera P u l l s e v e r a l f e e t of TV cable from MESA . (After completion of a r e s t period t h e LMP conducts environmental f a m i l i a r i z a t i o n , see S e c t i o n VIII) �CDR Remove camera from MESA: a. Pull the two pins at the forward edge of mounting frame b. Grasp TV handle and rotate TV toward rear of MESA to free from frame c. Lift camera from frame d. Check camera temperature and report (cold, normal, hot) Place camera on tripod. camera secure Check Carry camera with tripod to site to view subsequent EVA operations (See figure 3-4) Take a step-wise, fast-scan (10 frameslsec) panorama or, if time not available, select several points of interest. Do not point camera within 20" to sun. Start panorama at approximates 22" from an upsun view, move through down sun, continue to other view 22" from up sun. Place camera on surface for a few seconds at approximately 22 112" increments. (15 increments are required for the panorama) Recheck camera temp. and report. Place TV on surface for optimum coverage of surface activity (See Figure 3-4) Move near LMP. Restlcheck EMU. Check RCU. Report 02 and suit pressure. Photo SWC (stereo pair) after LMP deploys it. Return to MESA As required, pull more TV cable from MESA �LMP - CDR - VIII. LMP ENVIRONMENTAL FAMILIARIZATION (At t h i s p o i n t t h e CDR i s deploying t h e TV, s e e S e c t i o n VII) I n t h e v i c i n i t y of. l a d d e r and i n view of TV (and sequence camera, i f pract i c a l ) , check and r e p o r t balance/s t a b i l i t y : a. E f f e c t of CG s h i f t - l e a n forward, backward, and t o each s i d e b. Downward r e a c h c. A r m motion e f f e c t s E v a l u a t e and r e p o r t r e a c h c a p a b i l i t y (with and without support): a . Right up b Right down c. Both up and down . NOTE: Perform f o l l o w i n g e v a l u a t i o n s w i t h i n a few yards of SIC and i n view of sequence camera, i f practical E v a l u a t e and r e p o r t walking capability: a. b. c. d. Pace Stability Traction General e v a l u a t i o n ~ e s t / c h e c kEMU. Check RCU. Report oxygen and s u i t p r e s s u r e . Report p h y s i c a l comfort. Assess EVA capability �CDR - LMF' SWC DEPLOYMENT (At t h i s time t h e CDR is dep l o y i n g t h e TV, s e e S e c t i o n VII) a E r e c t SRC t a b l e : . . a. P u l l Velcro t a b s t o free table b. P u l l t a b l e forward from stowed p o s i t i o n and r o t a t e i n t o horizontal position c. Attach Velcro t a p e t o hold t a b l e i n correct position ( l e v e l , f o r e and a f t ) P u l l t h e two s t r a p s h o l d i n g SWC and remove SWC from MESA Walk t o s u n l i t a r e a Deploy SWC: a. Extend each s e c t i o n of s t a f f u n t i l i t l o c k s . ( r e d band should b e v i s i b l e ) Apply a compressing f o r c e t o each s e c t i o n t o check s e c t i o n s locked b. Extend shade c y l i n d e r and r o t a t e toward r e d s i d e of p i v o t p o i n t , i.e., r e d t o red c. Extend f o i l shade and hook t o lower p o r t i o n of s t a f f d. P r e s s s t a f f i n t o surf a c e w i t h f o i l normal t o sun ( s i d e marked SUN t o Sun) �CDR - LMP X. EVA AND ENVIRONMENT EVALUATION Remove camera from MESA and t e t h e r when r e q u i r e d i n t h e following evaluation NOTE: The f o l l o w i n g l i s t of t a s k s i s p r e s e n t e d a s a guide. The a c t i v i t i e s w i t h i n t h i s p e r i o d are n o t l i m i t e d t o t h e items l i s t e d o r t h e o r d e r i n which they appear. I f necessary f u r t h e r e v a l u a t e: a. E f f e c t of CG s h i f t b (leaning, reach, e t c . Walking capability .) I n u n d i s t u r b e d a r e a and i n view of TV a n d . SC, i f p r a c t i c a l , observe and report : a. Best pace b. Technique f o r s t a r t i n g and s t o p p i n g c. Balance a t i n c r e a s e d pace and l e n g t h of s t e p d. T r a c t i o n e. Dust f . Boot p e n e t r a t i o n ( t a k e stereo pair) g. S c u f f i n g h. Cohesion i. Adhesion (photo boots) 3 . General e v a l u a t i o n of EVA capability �CDR - I n each d i r e c t i o n , up sun, down sun and c r o s s sun, observe and r e p o r t s u r f a c e : a. b. c. d. e. f. Brightness/reflections Color p e r c e p t i o n Contrast v a r i a t i o n Texture determination R e f l e c t i o n i n shadow Rock and c r a t e r distribution g. General t e r r a i n evaluation h. Visual and t e r r a i n phenomena d i f f e r e n t from t h a t expected Check EMU s t a t u s w i t h MSFN af t e r stay i n sunlight. Report comfort /problems Move t o shadow edge and repeat l i g h t i n g / v i s i b i l i t y and t e r r a i n e v a l u a t i o n a s above. A d d i t i o n a l l y , observe shadow edge sharpness (look down sun) Check EMU s t a t u s w i t h MSFN a f t e r stay. Take 12 photo panorama (from p o s i t i o n 20 f e e t i n f r o n t of +Z pad). A s panorama is taken, e s t i m a t e d i s tance t o s e v e r a l prominent terrrain features. Repeat e v a l u a t i o n , a s above, i n shadow Check EMU af t e r s t a y i n shadow �CDR - LMP XI. BULK SAMPLE COLLECTION (The LMP i s conducting t h e EVA and Environment E v a l u a t i o n , S e c t i o n X) Remove camera and p l a c e on MESA P r e p a r e MESA: a. Proceed t o MESA b. I n s u r e a r e a about MESA is s u i t a b l e f o r operations c. Adjust h e i g h t of MESA, i f required d. I n s u r e a l l equipment i s accessible Deploy ETB: a. Unfold and p o s i t i o n bag on r i g h t s i d e of MESA (Check bag t o p f o l d e d i n s i d e bag) . P r e p a r e SRC and ALHT: a. Unstow scoop and hammer. P l a c e i n ETB b. Check s e c u r i t y of SRC t a b l e c. Release b u l k sample SRC c a r r y h a n d l e from d e t e n t p o s i t i o n d. R o t a t e h a n d l e 90' clockwise t o r e l e a s e SRC from MESA e. P u l l p e r p e n d i c u l a r t o MESA t o p w i t h c a r r y handle t o remove from stowage p o s i t i o n f . P l a c e SRC on t a b l e w i t h T-handle up and SRC a l i g n e d with t h e t a b l e g. R o t a t e and p l a c e t h e SRC on t a b l e w i t h SRC h a n d l e pointing away from t h e s p a c e c r a f t h. Release t h e two s t r a p l a t c h e s by p r e s s i n g t h e l a t c h l o c k i n g mechanism, w i t h t h e hand on t h e r e l e a s e handle, i n a sideways motion toward t h e c e n t e r of t h e SRC and r o t a t i n g t h e handle forward and upward . �i. Continuing t o grasp second . s t r a p l a t c h r e l e a s e handle, a f t e r relase, rotate the SRC top to' a n open s t a b l e ' p o s i t i o n . NOTE: I f necessary r e s t r a i n SRC with o t h e r hand on c a r r y handle i n order t o break seal j. Check t h e seal s p a c e r is s t i l l i n p l a c e over t h e s e a l k. Unpack SRC. P l a c e packing m a t e r i a l , and s m a l l sample bags i n SRC l i d , i n t r a n s f e r bag o r on MESA 1.. Remove s p r i n g s c a l e m. Hook s c a l e t o l e f t f r o n t of MESA n. Attach l a r g e sample bag t o s c a l e o. P l a c e SWC stowage bag i n SRC l i d o r on MESA NOTE: I f p r a c t i c a l c o l l e c t samples i n view of TV and sequence camera (NOTE: I f p r a c t i c a l use t h e scoop t o c o l l e c t rocks and loose m a t e r i a l simultaneously. Attempt t o c o l l e c t same volume of rocks a s loose m a t e r i a l ) C o l l e c t rock fragments: a. P u l l s t r a p t o f r e e v i b r a t i o n a t t e n u a t o r from tongs b. Remove t h e tongs from t h e MESA, p u l l t h e two lanyards t o r e l e a s e snaps c. Move w i t h i n s e v e r a l yards of t h e MESA t o c o l l e c t rock fragments placing each fragment i n t o t h e sample bag a t t h e t i m e of collection d. A t t h e completion of fragment sampling, place t h e tongs i n temporary stowage i n t h e MESA o r ETB �CDR R e s t l c h e c k EMU systems Collect loose material: a. Remove e x t e n s i o n h a n d l e from stowed p o s i t i o n on MESA. P u l l two snap l a n y a r d s on e x t e n s i o n h a n d l e t o r e l e a s e . Remove v i b r a t i o n a t t e n u a t o r from s m a l l handle. b. Remove scoop from ETB and connect t o e x t e n s i o n handle c . U s e scoop t o f i l l sample bag w i t h l o o s e m a t e r i a l . Comment on c o l l e c t i o n p r o c e s s , s o i l adhesion and cohesion, d i f f i c u l t y of ..scooping, volume of m a t e r i a l , general evaluation . d. Disconnect e x t e n s i o n handle . from scoop. P l a c e scoop 'and e x t e n s i o n h a n d l e i n temporary stowage on MESA o r i n ETB Res t l c h e c k EMU systems Pack and s e a l SRC: a. Remove sample bag from s p r i n g scale b. P l a c e sample bag i n SRC c. Close bag and p l a c e bag i n c e n t e r of SRC s o t h a t bag ends a r e toward SRC ends. d. P l a c e packing m a t e r i a l i n SRC t o minimize v o i d space U s e c a u t i o n t o keep SRC s e a l clean. e. Remove s e a l p r o t e c t o r . If a n O-ring s e a l is l o o s e , remove from SRC and d i s c a r d �CDR - LMP - f . Rotate t h e top closed with a s t r a p l a t c h handle g. S e a l t h e SRC by r o t a t i n g t h e two s t r a p l a t c h e s downward t o t h e locked p o s i t i o n ' P r e p a r e f o r SRC t r a n s f e r : a. R e t r i e v e LEC from stowed position b. Walk t o SRC c. A t t a c h LEC lower hook (marked w i t h "L") t o SRC t o p - l e f t f r o n t bracket d. Attach LEC upper hook (marked w i t h "R") t o t h e SRC t o p - r i g h t r e a r b r a c k e t and l o c k hook R e s t l c h e c k EMU XII. (At t h i s ' p o i n t t h e CDR i s comp l e t i n g t h e Bulk Sample Collect i o n , S e c t i o n XI) LM INSPECTION During i n s p e c t i o n e v a l u a t e v i s u a l perception Report s t a t u s of Quad I: a. Both LM s t a g e s (1) Coating (2) Dust (3) S h i e l d i n g b. Ascent s t a g e (one photo) (1) RCS (2) Rendezvous r a d a r c. Descent s t a g e (one photo) (1) Engine s k i r t , Report s t a t u s of +Z gear: a. Main s t r u t ( t a k e one photo) b. Secondary s t r u t s (two photos, one on each side) c. Take s t e r e o p a i r of padlsurf ace �Photo a r e a where b u l k sample was c o l l e c t e d Deploy ALSCC : (Deployment of t h e ALSCC w i l l b e delayed u n t i l t h e documented sample c o l l e c t i o n i f behind i n the timeline) . a. Remove i s o l a t o r l a t c h p i n and p i v o t cover b. P u l l camera from MESA c. P l a c e camera on secondary g e a r s t r u t and e x e r t . p r e s s u r e on camera cover. P u l l t h e two s k i r t l a n y a r d s d. R o t a t e handle r e t a i n i n g latch e. Swing handle clockwise 150° and p u l l u n t i l f u l l y extended f . P l a c e camera on s u r f a c e ALSCC OPERATION Close-up photographs w i l l b e t a k e n by e i t h e r crewman when time i s a v a i l a b l e between or during other tasks. Several times w i t h i n t h e EVA a r e sugg e s t e d when i t may b e convenient f o r t h e crew t o t a k e photos. T h i s i s n o t a requirement t o t a k e photos nor does i t p r o h i b i t . them from o b t a i n i n g photographs a t o t h e r times which may b e feasible. I n g e n e r a l t h e camera o p e r a t i o n is : a. Estimate p o s i t i o n of o b j e c t p l a n e r e l a t i v e t o camera bearing surface b. P o s i t i o n camera over o b j e c t (Describe o b j e c t and l o c a t i o n ) , �CDR - c. I f o b j e c t is below ALSCC bearing surface depress s k i r t u n t i l o b j e c t i s w i t h i n focus plane d. I f o b j e c t is above b e a r i n g s u r f a c e t i l t camera back u n t i l o b j e c t i s w i t h i n focus p l a n e e. A c t i v a t e t r i g g e r l o c a t e d on handle g r i p f . Read and r e p o r t frame c o u n t e r g. Observe c y c l e completion by l i g h t on handle Carry t h e ALSCC around t h e LM d u r i n g t h e i n s p e c t i o n and t a k e photos a s p r a c t i c a l Report s t a t u s of Quad IV: a. Both LM s t a g e s (1) Coating (2) Dust (3) S h i e l d i n g b. Ascent s t a g e (1) RCS (2) St e e r a b l e antenna (3) Rendezvous r a d a r c. Descent s t a g e (1) Descent engine s k i r t (2) MESA Report s t a t u s of +Y g e a r assembly: a. Main s t r u t b. Secondary s t r u t s . Take one photo of A/S Take one photo of s k i r t Take one photo of MESA ( I n c l u d e a l l Quad I V , i f practical) Take one photo of main s t r u t Take two photos, one on each s i d e of secondary s t r u t s Take s t e r e o p a i r of pad/ surface �CDR R e s t l e v a l u a t e and r e p o r t l i g h t i n g / v i s i b i l i t y i n a l l directions, p a r t i c u l a r l y SIC r e f l e c t i o n s . Observe and r e p o r t t e r r a i n c h a r a c t e r i s t i c s . Estimate dist a n c e t o s e v e r a l prominent t e r r a i n f e a t u r e s . Take close-up photos i f p o s s i b l e - .LMP Take panorama (12 photos) from p o s i t i o n approx 20 f t o u t from +Y pad and 30 deg CW from +Y a x i s o r 120 deg from l a s t panorama Report s t a t u s of Quad 111: a. Both LM s t a g e s (same a s Quad IV) b. Ascent s t a g e (1) RCS (2) St e e r a b l e antenna (3) VHF antenna c. Descent s t a g e (1) P r o p e l l a n t v e n t s (2) F u e l v e n t (3) Tanks (Oxygen, Helium (2)) (4) Descent engine s k i r t (5) Note i f s u r f a c e d i s c o l o r e d Report s t a t u s of -Z g e a r assembly (same items a s +Y and: Take one photo of A/S , Take one photo of s k i r t (Photo i f s u r f a c e d i s c o l o r e d ) Take same photos a s +Y a. Landing t r a c k b. O x i d i z e r v e n t c EVA antenna) . . Receive camera and t e t h e r t o s u i t Hand Hasselb l a d camera t o CDR Report s t a t u s of Quad 11: (The LMP b e g i n s t h e . EASEP deployment. See t h e following s e c t i o n ) a. Both IN s t a g e s (same a s Quad IV) b. Descent s t a g e (one photo) (1) Landing r a d a r (2) SEQ bay ' T a k e 12 photo panorama (from 20 f t o u t from -Y pad and 30' CCW from -Y a x i s o r 120' from l a s t panorama position) �CDR - LMP Report s t a t u s of -Y g e a r assembly: a. Main s t r u t ( t a k e one photo) b. Secondary s t r u t s (one photo from each s i d e ) c. P a d l s u r f a c e ( t a k e s t e r e o pair) XIII. (At t h i s p o i n t t h e CDR i s completing t h e LM i n s p e c t i o n . See t h e precedi.ng s e c t i o n ) NOTE: I f LMP cannot r a i s e door, s t a n d c l e a r of d o o r , a n d manually' a s s i s t ' EASEP DEPLOYMENT Open SEQ bay door: a. Remove thermal cover from door lanyard b. R e t r i e v e l a n y a r d from r i g h t s i d e of SEQ bay (remove lower v e l c r o strap) c. Move t o p o s i t i o n c l e a r of door d. p u l l w h i t e of lanyard t o r a i s e door e. Temporarily stow lanyard on s t r u t f . I f Quad I1 is i n a low a t t i t u d e connect f o l d e d doors w i t h v e l c r o s t r a p PACKAGES REMOVED BY BOOMS Photograph package removal Remove Package 1 (PSE): a. R e t r i v e boom l a n y a r d from package, (handle) . ' . b. Move t o p o s i t o n c l e a r of package (approximately . . 10 f e e t ) c. P u l l w h i t e p o r t i o n of lanyard t o unlock and move package from SEQ bay t o f u l l y extended boom position �CDR - LMP d. P u l l b l a c k and w h i t e s t r i p e d p o r t i o n of lanyard t o lower package t o s u r f a c e e. R e l e a s e w h i t e p o r t i o n of lanyard from b a s e of package f . P u l l s m a l l lanyard ( v e l c r o e d t o handle) on package t o r e l e a s e boom c a b l e and l a n y a r d s . Reattach lanyard t o v e l c r o g. Move package c l e a r h. P u l l b l a c k and w h i t e s t r i p e d lanyard t o r e t r a c t boom ( o r push boom back w i t h hand) Remove Package 2 (LR') : a. Repeat Package 1 procedure ( s e t package c l e a r of SEQ bay MANUAL PACKAGE REMOVAL Remove Package 1: . a. P u l l s m a l l l a n y a r d , a t t o p o r bottom of package, t o r e l e a s e hockey s t i c k from boom b. Remove deployment l a n y a r d from package and p u l l w h i t e p o r t i o n t o unlock package from bay c. Release w h i t e p o r t i o n of lanyard from b a s e of package d. Move deployment l a n y a r d t o s i d e c l e a r of package e. Manually p u l l package c l e a r of SEQ bay f . S e t package on s u r f a c e c l e a r of bay a r e a �LMP - CDR - Remove Package 2: a. Repeat Package 1 procedure NOTE: Simultaneous accomplishment, although i n d i c a t e d of t h e following tasks, is not required. Photo LMP and t a k e close-up photos a s p r a c t i c a l Close SEQ bay door: a. R e t r i e v e door l a n y a r d b. Move t o p o s i t i o n c l e a r of door c. P u l l b l a c k and w h i t e s t r i p e p o r t i o n of l a n y a r d u n t i l door is c l o s e d d. Discard l a n y a r d . 3 S e l e c t s i t e f o r PSE and LR deployments, nominally 70 f t s o u t h of t h e SIC . Move to'deployment s i t e w i t h cameras. E s t i m a t e d i s t a n c e and p o s i t i o n w i t h r e s p e c t t o t h e LM P l a c e LR3 w i t h b a s e toward Earth. (Astronaut f a c e s e a s t f o r S i t e s 1 and 2 and west f o r S i t e s 3,4, and 5). R e s t / prepare a r e a ( c l e a r rocks, smooth s u r f a c e as r e q u i r e d ) 3 Carry PSE and LR t o deployment s i t e (Nominally 70 f e e t out t h e LM-Y a x i s . Report s i t e 10cat i o n i f i t is n o t nominal) 3 P l a c e LR package on s u r f a c e (on end) i n a c l e a r , l e v e l l o c a t i o n , i f p r a c t i c a l . Move PSE approximately 1 0 f e e t f u r t h e r from T.,M and p l a c e on s u r f a c e w i t h b a s e toward n o r t h (Arrow on handle p o i n t s t o south) 3 Deploy LR : a. Simultaneously g r a s p deployment boom ("hockey s t i c k " ) and p u l l p i n ' i n s i d e c a r r y handle. Remove and d i s c a r h "hockey s t i c k " a* Res t / c h e c k EMU �CDR b . ment Simultaneously g r a s p deployh a n d l e and r e l e a s e r i n g c. d. e. f. . * ( L e f t s i d e of package) t o release deployment handle p u l l pin O P u l l deployment handle t o extend handle s i x inches, t o the f i r s t d e t e n t p o s i t i o n , and t o p a r t i a l l y r e l e a s e a r r a y . Discard handle release ring Grasp p u l l r i n g on a r r a y t i l t i n g handle, p u l l t o remove p r o t e c t i v e cover. Discard cover @ Grasp deployment handle t o s t e a d y package. @ Grasp a r r a y t i l t i n g handle, push down r o t a t e handle 45'. P u l l outward t o extend t o d e t e n t p o s i t i o n (9.5 i n c h e s ) and complete a r r a y r e l e a s e @ Use deployment handle t o s t e a d y package. Use a r r a y t i l t i n g handle t o t i l t a r r a y ( t o d e t e n t f o r landing s i t e ) Deploy PSE: a. P r e p a r e a r e a (move r o c k s , . etc.) i f required b. From b a s e of package p u l l l a n y a r d t o r e l e a s e gnomon @ c. Grasp c a r r y h a n d l e w i t h one hand and u s e t h e o t h e r t o remove and d i s c a r d t h e r i g h t s o l a r panel-restraini n g p u l l p i n @ and p a n e l support bracket p u l l p i n @ d. Grasp f i r s t s o l a r p a n e l support bracket, r o t a t e b r a c k e t forward l i f t b r a c k e t upward t o r e l e a s e and remove f i r s t r e a r support bracket-p u l l pin. @ Discard b r a c k e t / l a n y a r d / p u l l p i n The c i r c l e d numbers and symbols correspond t o d e c a l s on t h e packages. g. R e l e a s e t i l t i n g handle (should s p r i n g back i n t o stowed position) h. Depress t r i g g e r on deployment handle, p u l l handle t o extend t o f u l l @ e x t e n t (an a d d i t i o n a l 27 inches) and r o t a t e package t o lunar surface i. Check and r e p o r t experiment a l i g n e d and l e v e l t o w i t h i n Use gnomon +5O. - @1-1 shadow c a s t on p a r t i a l compass r o s e f o r alignment. Use bubble f o r l e v e l i n d i c a t i o n . Use deployment h a n d l e t o a l i g n and l e v e l as r e q u i r e d e. Repeat procedures c. and d. f o r t h e l e f t s o l a r panel bracket @ @ @ f . From s i d e of PSE p u l l deployment h a n d l e ("worki n g height") p i p p i n @ and remove "hockey s t i c k " @ g. Grasp deployment h a n d l e , r o t a t e and p u l l t o extend t o 30 i n c h working h e i g h t and l o c k i n p l a c e @ h. Use deployment handle t o r o t a t e package t o s u r f a c e i. With deployment h a n d l e , embed package mounting t a b s i n l u n a r s u r f a c e (smooth s u r f a c e and a l i g n package) 0 ~nm-1 �CDR - Photograph s c i e n t i f i c packages: CAUTION : Do n o t walk up-sun of t h e PSE. Shadows on t h e s o l a r p a n e l s affect internal electronics a. Take c l o s e u p photo of LR3 b. Take s t e r e o p a i r of LR3 c. Take one photo from about same distance a s stereo p a i r but a t e n t i r e l y d i f f e r e n t angle d.. Move t o PSE e. Repeat photos as i n a , b , and c j. Check and r e p o r t experiment a l i g n e d and l e v e l t o withi n i-5' a s i n d i c a t e d by gnoKon shadow c a s t on part i a l compass r o s e and bubble l e v e l , r e s p e c t i v e l y . Use deployment h a n d l e t o a l i g n and l e v e l as r e q u i r e d . k. P u l l antenna r e l e a s e lanyard from deployment handle ( v e l c r o e d t o handle) 1. P u l l l a n y a r d t o deploy s o l a r p a n e l s and antenna NOTE: . I f p a n e l s do n o t deploy, s t a n d c l e a r of deployment a r e a and check r e a r s u p p o r t b r a c k e t s c l e a r of s o l a r p a n e l s and r e l e a s e l e v e r s (underneath forward edge of p a n e l s ) p u l l e d m. R o t a t e antenna t o designated landin o f f s e t ( s i t e dependent) n. Recheck package l e v e l and a l i g n e d . Report shadow on compass r o s e &) Move t o t h e Quad IV a r e a Move t o MESA w i t h ALSCC.: Take photos a s p r a c t i c a l . Photo f o o t p r i n t made w h i l e c a r r y i n g EASEP R e s t l c h e c k EMU Restlcheck EMU XIV. ~ e s t / p h o t oLMP. close-up photos Take ' - DOCUMENTED SAMPLE COLLECTION T r a n s f e r b u l k sample SRC t o footpad o r g e a r s t r u t s : . . a. Extend loop end of LEC u n t i l s e c t i o n of s t r a p going t o A/S i s t a u t .b. L i f t SRC from t a b l e by l e f t (lower) hook @ �CDR c. Carry SRC and p l a c e on footpad o r secondary struts d. Temporarily stow LEC on gear s t r u t e. Return t o MESA P r e p a r e documented sample SRC f o r sample c o l l e c t i o n : a. Check s e c u r i t y of t a b l e b. P u l l t h e lanyard on l e f t s i d e of TV mounting b r a c k e t t o r e l e a s e t h e two p u l l pins. c. Remove and d i s c a r d b r a c k e t under LM d. Release DS SRC c a r r y h a n d l e from d e t e n t p o s i t i o n e. R o t a t e handle 90' clockwise t o r e l e a s e SRC from MESA f . P u l l perpendicular t o MESA top w i t h c a r r y h a n d l e t o remove from stowage position g. P l a c e SRC on t a b l e w i t h T-handle up and SRC a l i g n e d with the t a b l e h. R o t a t e and p l a c e . t h e SRC on t a b l e w i t h SRC handle p o i n t i n g away from t h e spacecraft i. Release t h e two s t r a p l a t c h e s by p r e s s i n g t h e l a t c h l o c k i n g mechanism w i t h t h e hand on t h e r e l e a s e handle i n a sideways motion toward t h e c e n t e r of t h e SRC and r o t a t i n g t h e handle forward and upward �CDR j. Continuing t o g r a s p second strap latch release handle, a f t e r r e l e a s e , r o t a t e t h e SRC t o p t o an open s t a b l e p o s i t i o n . NOTE: I f necessary res t r a i n SRC w i t h o t h e r hand on c a r r y h a n d l e i n o r d e r t o break s e a l k. Check t h e s e a l s p a c e r i s s t i l l i n p l a c e over t h e bottom s e a l 1. Remove and stow packing m a t e r i a l on SRC l i d , o r i n MESA o r ETB Remove one c o r e t u b e from SRC and p l a c e i n SRC l i d o r ETB . n. Remove t u b e caps and p l a c e i n SRC l i d (two caps . . . wrapped i n packing m a t e r i a l ) 0. Remove small sample bag c o n t a i n i n g York mesh. S e a l bag and p l a c e i n SRC l i d Walk t o LMP ', C o l l e c t c o r e t u b e sample: Take s t e r e o p a i r a f t e r t u b e i s pushed i n t o s u r f a c e ' a. Remove c o r e t u b e from SRC (check b i t a t t a c h e d ) and connect t o t h e e x t e n s i o n handle b. Remove hammer from ETB c. Move t o an u n d i s t u r b e d p o i n t n e a r t h e MESA ( i n view of TV, i f p r a c t i c a l ) d. P l a c e t h e c o r e t u b e a t t h e sampling l o c a t i o n . Push tube i n t o surface t h e l e n g t h of t h e tube. Drive w i t h t h e hammer i f n e c e s s a r y e. R e t r i e v e t u b e by p u l l i n g a l o n g its vertical axis, rotating i f necessary �CDR - I f procedure above i s n o t p r a c t i c a l o r i f t i m e perm i t s , p l a c e gnomon n e a r p r o s p e c t i v e fragment and/or s o i l sample ( n e a r s e v e r a l samples i f p o s s i b l e ) and t a k e two photos of sample s i t e . From approximately f i v e f e e t away, t a k e two photos ( s t e r e o p a i r ) from n e a r 90' t o sun l i n e NOTE: The types of samples and t h e o r d e r i n which they a r e coll e c t e d w i l l b e dependent on t h e t e r r a i n features investigated and crew judgement on t h e b e s t i n v e s t i g a t i v e approach w i t h i n operational limitations. . . Remove a s m a l l b a g ( s ) from l a r g e bag. Report number on bag. (Bags a r e numbered 1 through 14) Open s m a l l bag and hold f o r LMP S e a l small bag and p l a c e i n i n l a r g e c o l l e c t i o n bag Photograph a r e a ( s ) where sample(s) was taken C o l l e c t sample(s) w i t h scoop o r tongs. P l a c e i n bag ( c o l l e c t s e v e r a l samples i f possible) NOTE: The scoop can be used t o simultaneously.collect a small fragment and a s m a l l q u a n t i t y of l o o s e m a t e r i a l S e l e c t a n o t h e r sample and d e s c r i b e o r s e l e c t a new sample a r e a Pick up gnomon ( i f gnomon cannot be conveniently included i n photographs of n e x t sample) �CDR - I f procedure above i s n o t p r a c t i c a l o r i f t i m e perm i t s , p l a c e gnomon n e a r p r o s p e c t i v e fragment and/or s o i l sample ( n e a r s e v e r a l samples i f p o s s i b l e ) and t a k e two photos of sample s i t e . From approximately f i v e f e e t away, t a k e two photos ( s t e r e o p a i r ) from n e a r 90' t o sun l i n e NOTE: The types of samples and t h e o r d e r i n which they a r e coll e c t e d w i l l be dependent on t h e t e r r a i n features investigated and crew judgement on t h e b e s t i n v e s t i g a t i v e approach w i t h i n operational limitations. . . Remove a s m a l l bag(s) from l a r g e bag. Report number on bag. (Bags a r e numbered 1 through 14) Open s m a l l bag and hold f o r LMP S e a l s m a l l bag and p l a c e i n i n l a r g e c o l l e c t i o n bag Photograph a r e a ( s ) where sample(s) was taken C o l l e c t sample(s) w i t h scoop o r tongs. P l a c e i n bag ( c o l l e c t s e v e r a l samples i f possible) NOTE: The scoop can be used t o simultaneously.collect a small fragment and a s m a l l q u a n t i t y of l o o s e m a t e r i a l S e l e c t a n o t h e r sample and d e s c r i b e o r s e l e c t a new sample a r e a Pick up gnomon ( i f gnomon cannot be conveniently included i n photographs of next sample) �CDR Move t o a new sampling a r e a Repeat sampling procedure a t new s i t e ( s ) - u n t i l t h e c o l l e c t i o n bag is f i l l e d o r t h e a l l o t t e d time h a s elapsed. ~ e s t l c h e c kEMU as a p p r o p r i a t e . Take s u r f a c e close-up photographs i f feasible Move t o MESA w i t h s t i l l and close-up cameras Move t o MESA w i t h tongs, scoop, and samples Remove ALSCC f i l m c a s s e t t e and stow: a . P u l l t h e two cover l a n y a r d s and remove cover b. R o t a t e c a s s e t t e f i l m cutter lever c. L i f t c a s s e t t e r e t a i n i n g arm d. Remove c a s s e t t e a n d . p l a c e i n CSC pocket on CDR's s u i t . Close CSC pocket Remove l a r g e sample bag from LMP and a t t a c h t o s p r i n g s c a l e on MESA P l a c e scoop by o r on MESA Hold c o n t a i n e r f o r LMP Hand c o n t a i n e r t o CDR Remove sample of t h e i n the Remove t h e environmental container, the l a r g e r two s m a l l c o n t a i n e r s SRC, and open. o-ring from s e a l �CDR Use scoop to collect loose material from an undisturbed area where bulk sample was taken. Place sample in container. Place scoop by MESA Seal container and place in SRC Remove the gas analysis container from SRC and open. Remove o-ring seal Hand container to CDR Hold container for LMP Use tongs to collect a small rock fragment from bulk sample area and place in container. Seal container and place in SRC Detach tongs and place in ETB Recover SWC: Use scoop to collect rocks and loose material. Fill large sample bag to designated weight or volume Move to SWC Withdraw staff from surface Roll up foil Rotate foil roller to detach position and remove from staff Let staff rest on surface, vertically and with only its weight acting on surface, report depth of penetration Push staff into surface as deep as possible Assess amount of force applied and staff depth If time permits photograph staff and repeat e and f several times. Check staff rigidity in surface Carry SWC foil to MESA Place bag in SRC. Seal bag Remove SWC bag from temporary stowage on MESA and open Hold bag for CDR Insert foil into bag Seal SWC bag and place in SRC Collect second core tube sample if time available (See procedures on page 55) If time not available assist CDR Place York mesh sample (in SRC lid) in SRC. Place packing material in SRC to minimize void space 68 �CDR - T r a n s f e r b u l k sample SRC and magazine: ( I f t h e r e i s time f o r t h e t r a n s f e r of only one SRC, t h e b u l k sample SRC w i l l be t r a n s f e r r e d ) a . Extend loop end of LEC u n t i l s e c t i o n of s t r a p going t o A/S i s t a u t b. Grasp loop g r i p on t h e LEC top l i n e c. L i f t SRC from s t r u t d. Walk t o t h e f r o n t of t h e . l a d d e r w i t h SRC suspended on LEC e. Walk away from l a d d e r ( i n +Z d i r e c t i o n ) w h i l e h o l d i n g LEC t o p . s t r a p (loop) t o t r a n s f e r magaz i n e and SRC t o A/S Assist CDR, i f r e q u i r e d Disconnect and t e m p o r a r i l y stow SRC and camera magazine P r e p a r e f o r t r a n s f e r of documented sample SRC: a. P u l l LEC lower l i n e t o t r a n s f e r LEC hooks t o surface b. With LEC hooks i n hand, walk t o SRC on MESA c. Attach LEC lower hook t o SRC t o p - l e f t f r o n t b r a c k e t and l o c k hook d. A t t a c h upper ( r i g h t ) hook t o SRC t o p - r i g h t r e a r b r a c k e t and l o c k hook T r a n s f e r SRC: a. Extend loop end of LEC u n t i l s e c t i o n of s t r a p going t o A/S i s t a u t b. Grasp LEC t o p l i n e by loop g r i p �CDR - c. L i f t SRC from t a b l e d. Walk t o t h e f r o n t of t h e l a d d e r w i t h SRC suspended on LEC e. Walk away from l a d d e r ( i n +Z d i r e c t i o n ) w h i l e h o l d i n g LEC top s t r a p loop t o t r a n s f e r SRC t o A/S A s s i s t CDR, i f r e q u i r e d ~ e s t l c h e c kEMU Disconnect and t e m p o r a r i l y stow SRC XVII. CDR EVA TERMINATION Clean EMU by d u s t i n g w i t h hands and wiping o r k i c k i n g b o o t s a g a i n s t footpad Change SC FR t o 1 2 / s e c Ascend t o p l a t f o r m Disconnect LEC from ascent stage Receive and d i s c a r d end of LEC away from LM Hand end of LEC through h a t c h t o CDR Ingress A s s i s t CDR, i f r e q u i r e d J e t t i s o n ECS c a n i s t e r and b r a c k e t , OPS b r a c k e t s (adapt e r s ) , 3 a r m r e s t s , bag of used u r i n e bags Close h a t c h Repressurize cabin �SECTION 4.0 ALTERNATE AND CONTINGENT PLANS �4.0 ALTERNATE AND CONTINGENT PLANS 4.1 Alternate EVA (With S-band Erectable Antenna ~eployment) An alternate timeline is presented for the situation in which deployment of the S-band erectable antenna is required. Such a situation will occur if the Goldstone or Parkes (~ustralia) 210-foot antennas are not in view and the communications capability with the LM steerablel85-foot antenna combination is not sufficient to simultaneously obtain acceptable W coverage and voice-biomedical and telemetry data. Thus, due to the present uncertainty of the communications capability - possible unsatisfactory equipment performance and/or contingencies which may cause mission event times to vary so that a 210-foot antenna is not in view, the erectable antenna will be carried on the mission and a real time decision made to deploy or not deploy it, i.e., follow the alternate or the nominal timeline. With the addition of the erectable antenna deployment, the major impact to the timeline is the reduction of time available for the documented sample collection. Also, for the alternate timeline, the LMP must delay his egress to switch to the erectable antenna after the CDR has deployed it. �4.1.2 WITH DEPLOYMENT OF S-BAND ERECTABLE ANTENNA SUMMARY TIMELINE ALTERNATE LUNAR SURFACE EVA b t r r ~ v ~ corm r a rvr I I �1.50 2 a00 2r10 2.20 2.40 1.30 ...t..,..r*............... ...................................................... ................................................. z; I P ~ CSI o o c u r r r r r o s ~ u r r rc o r r c c r ~ o r LY* *.ESTPMOIO ng .OVU6MT 1 S11C *l..I C L O I I . " I .OCPLW LI'EXP. .IOIO I I I ElKlUL.IS ursrm 0 r o* . . j 1c. TO rue 0 5 Ale& o"0,r SlYPLI I c ~ ~ t c r ~ o r *lclalCVE sru L ,L". , " I . , Slit ' 11~. t o OZPLOI .KROl 01 .. 1.50 snrr ICLOSIY. .cL~." I E Y 1 ICRYIWIIO~ CYU YYPLE ."*I101 L ~ r c a c s sc r s l m ! 0C"rcl IOOLS ru .OUK.TC b c o r ~ e r SIYOLES .PAC" YYeLIs Rwros 2.00 CWIPYIII marc* U141SS Cllll I I I I I I I 7U.C PASSNC S C l S W U P . 1 C.011 *JElItSOll .SCCUIC j SCI ,IIST.RIOlO .nr.uc 0s C S. e n n s r c a o r sac I Am0 S f O l 5% LADDIm *t.Cacss I *CLOSC EYY *A%tW I CWUO. o o c v v c n l t o wrrrr c m r r c r ~ o m * m v c l V L l SIC 1 0 .CLCA# AMD SIOLL I * S T 0 1 LLSCC r l l Y Y O T O S.r.LImG *rcr*re wuprc (1YEl.S t~.hvra f::rt;it*m8&L;M~C PDros 2.10 . I I . i I sra crvenr lltCCIYt u.cul"c 8 SIW V C . jI bI ltCElVE sac 2 rJ0 2.30 2.40 �4.1.3 ALTERNATE TIMELINE LUNAR SURFACE EVA CDR HRtMIN LMP - LMP - CDR - II + %R MONITOR ACTIVITY PLAY OUT LEC MOVE TO POSITION AND RELEASE MESA 1 I I t + TV ON FOR CHECK* START SEQUENCE CAMERA (SC) + DESCEND TO FOOTPAD CHECK ASCENT PROCEDURES PLAY O ~ LEC T I TURN TV ON '(AND OFF)* CHANGE SC FR TO 24/SEC I CHANGE SC FR TO 121SEC STOW LEC T STEP TO SURFACE RESTICHECK EMU 4- + I T VISUALLY MONITOR CDR A C T I V I T Y PROVIDE CHECKLIST ASSISTANCE CHECK AND DISCUSS BALANCElSTABIL I T Y WALKING CAPABILITY *TV LEFT ON I F SATISFACTORY 1 , TELEMETRY AND CHANGE SC F I L M MAG VOICE-BIOMED CHANGE FR, TO 6/SEC 1- DATA RECEIVED A II I CDR LEC ' MISSION I APOLLO 11 I EDITION FINAL I 1 DATE 1 JUNE 27, 1 9 6 9 MISSION TIME 112+30 - 112+54 I DAY/ REV 5/19 I W6E 1 of 7 I �ALTERNATE TIMELINE CDR HRtMIN LMP T + RESTICHECK EMU I I 6 T DEPLOY HANDLE I EXTEND BAG COLLECT SAMPLE 4DETACH BAG AND LMP - REMOVE S-BAND ERECTABLE AIITEliNA FROM S/C CHECK LM-L AND EMU $TART sc t UNSTOW CSC AND - CDR II CtiECK LM AND EMU I t CHANGE CARRY ANTENNA TO DEPLOYMEiVT S I T E SC% TO B/SEC I MONITOR CDR ACTIVITY t ORIENT ANTEIIIjA REMOVE TOP CAP DISCARD HANDLE -L I I STOW SAMPLE t I TRANSFER S T I L L CAMERA TO SURFACE PROVIDE CHECKLIST ASSISTANCt EXTEND MAST AND LEGS PREPARE FOR CAMERA TRANSFER ASSIST CDR C I + REMOVE THERMAL COVER AND L I F T ANT. ONTO LEGS CHANGE SC FR TO 11SEC + REMOVE DEPLOY BAR AND R I B T I P PROTECTOR t CHECK AND REPORT LM STATUS 3- I CHAijGE SC FR TO l / S k C OPEN ANTENNA D I S H I t MONITOR CDR ACTIVITY PROVIDE CHECKLIST ASSISTANCE t CHECK TERRAIii ANij LIGHTING t REMOVE CABLE FROM MESA MONITOR CDR A C T I V I T Y I 1, MISSION AF'OLLO 11 I I EDITION FINAL I I I DATE JUNE27,1969 MISSION TIME 112+54-113+18 I DAY/ IW 5/20 I PAOE 2 of 7 �ALTERNATE TIMELINE CDR - LMP - LMP CDR - II T t T ATTACH CABLE TO ANTENNA STEP TO SURFACE REST/CHECK EMU CHANGE SC F I L M MAG. t 1 ROUGH ALIGN ANTENNA I PREPARE MESA FOR TV DEPLOYMENT I MONITOR CDR A C T I V I T Y CHECK BALANCE/STABIL I T Y I REMOVE TRIPOD -1 I CHANGE FROM WA TO L D LENS S-BAND T ~ I L U N A RSTAY TURN ~ T VON CHECK COMM, LM, AND EMU DETERMINE "GO" FOR EVA PLACE SPARE CAMERA ON L L F L O O R REORIENT SC REST/CHECK COMM AND EMU I T + REMOVE CAMERA AND PLACE ON TRIPOD + CARRY TV TO DEPLOY S I T E MISSWN 1 EDITION FINAL I I JUNE 4 + MOVE NEAR LMP REST/CHECK EMU 27, 1969 REMOVE SWC' FROM MESADEPLOY I N SUNLIGHT + P H O T L SWC I DATE ERECT SRC TABLE PLACE TV FOR SUB. EVA CHECK ASCENT PROCEDURE rC, rC, t TAKE FAST SCAN PANORAMA OR SEVERAL POINTS OF, INTEREST t PERFORM COMM CHECK I I + + MONITOR AND DESCEND TO PAD PHOTO LMP PULL TV CABLE FROM MESA t MOVE THRU HATCH CHECK INGRESS PROCEDURE MONITOR AND PHOTO EGRESS APOLLO 11 I DETERMINE WALKING C A P A B I L I T Y MISSION TIME 113+18 - 113+42 I DAY1RN 5 /20 1 1 PAGE 3 of 7 i �ALTERNATE TIMELINE LMP PLACE CAME$ ON MESA PREPARE 'MESA FOR BULK SAMPLE COLLECTION t t PREPARE ALHT AND SRC LIGHTING/VISIBILITY AND TERRAIN I N SHADOW EVALUATE AND REPORT EVA CAPABILITY AND EFFECTS ON SURFACE (TETHER CAMERA WHEN REQUIRED) REST/CHECK EMU PHOTO QUAD I t I PACK SRC EVALUATE AND REPORT LIGHTING/VISIBILITY AND TERRAIN I N SUNLIGHT REPORT STATUS AND PHOTO +Z GEAR PHOTO BULK SAMPLE AREA I t REMOVE ALSCC FROM MESA AND DEPLOY CONNECT LEC I MISSION APOLLO 11 I I CARRY ' ALSCC REPORT STATUS QUADI I V EVALUATE AND REPORT LIGHTING/VISIBILITY AND TERRAIN AT SHADOW EDGE COLLECT ROCKS AND LOOSE MATERIAL 1. I I REPORT' STATUS +Y GEAR I I EDITION FINAL I PHOTO + EVALUATE T E R R A I N / V I S I B I L . I T Y TAKE PHOTO PANORAMA TAKE CLOSE-UP PHOTOS k I DATE ( JUNE 27, 1969 M I S S I O N TIME 113+42 - 114+06 I t I t PHOTO QUAD I V DAY/ REV 5/20 + Y GEAR I t TAKE PHOTO PANORAMA /I. I PAGE 4 of 7 1 �A L T E R N A TTIMELINE E LMP - CDR - I, PHOTO QUAD I11 CARRY C A ~ E R A STO DEPLOY S I T E REPORT POSITION FROM LM CDR LMP - 2: REPORT STATUS QUAD I11 I I t t 1 REPORT STATUS -Z GEAR PHOTO -Z GEAR + I CARRY PSE TO DEPLOY S I T E I t TRANSFER CAMERA TO CDR t I REPORT STATUS DEPLOY PSE PHOTO L R ~ OPEN SEQ BAY DOOR I I AND PHOTO QUAD 11- I' T PHOTO EASEP OFFLOAD MOVE TO PSE t t REPORT STATUS AND PHOTO -Y GEAR + PHOTO PSE + MOVE BULK SRC TO STRUTS OR FOOTPAD RESTIPH'OTO LMP TAKE CLOSE-UP PHOTOS REMOVE ALSCC F I L M AND STOW I N S U I T I DEPLOY S I T E APOLLO 11 1 MOVE MESA RESTICHECK EMU MOVE TO QUAD I V . I PHOTO EASEP OFFLOAD TAKE CLOSE-UP PHOTOS I TAKE CLOSE-UP PHOTOS REMOVE PACKAGE 2 ( L R ~ ) TAKE PHOTO PANORAMA MISSION t T REMOVE PACKAGE 1 (PSE) EDITION FINAL I 1 PREPARE DS SRC AND SAMPLING EQUIPMENT L I DATE JUNE 27, 1 9 6 9 MISSION TIME 114+06 - 114+30 I DAY/R€V 5/20 I PAG€ 5 of 7 I �r ALTERNATE TIMELINE LMP &C -L TETHER SA%E LMP - II ASCEND TO PLATFORM t BAG TO LMP COLLECT CORE TUBE SAMPLE UNSTOW GNOMON SELECT DS AREA MOVE TO DS AREA PHOTO DS AREA + LI t INGRESS I CHECK LM A N D EMU REMOVE S T I L L CAMERA MAGAZINE AND CONNECT TO LEC 1 T I REORIENT CAMERA DESCRIBE AND COLLECT SAMPLES . PHOTO SAMPLES AND SAMPLE AREA ASSIST LMP I t. 4- MOVE TO MESA PLACE SAMPLES I N SRC RETRIEVE AND STOQW C MOVE TO MESA PLACE TOOLS I N ETB PACK SRC CLOSE AND SEA; SRC MOVE TO' LADDER CLEAN EMU MISSION I APOLLO 11 1 I TRANSFER BULK SAMPLE SRC AND CAMERA MAG. I- 1 EDITION FINAL - I DATE C t DISCONNECT AND STOW SRC AND CAMERA MAG. REST/CHECK EMU I LOWER LEC I I JUNE 27, 1969 ASSIST 'CDR, I F REQUIRED 1 MISSION 114+30 - 114+54 DAY! REV 5/20-21 I PAOL 6 of 7 I �LMP CDR I JETTISON EQUIPMENT CLOSE HATCH 1 '"f CABIN REPRESS �4.1.4 Detailed Procedures Refer t o t h e Nominal Lunar EVA Detailed Procedures Section 3.5, f o r t h e procedures which precede t h e S-band Erectable Antenna Deployment. LMP - CDR - S-BAND ERECTABLE ANTENNA DEPLOYMENT Transfer antenna t o deployment s i t e : . a. Walk t o antenna stowage p o s i t i o n ( ~ u a dI ) . . b . Remove thermal s h i e l d c . Remove Velcro s t r a p s and p u l l t o r e l e a s e p i n s a t base of antenna d. Grasp antenna- by deployment . "shimmy" b a r and folded l i f t handle ' e . P u l l antenna o u t and down by l i f t handle t o c l e a r LM s t r u c ture f . Hold antenna by deployment b a r and deploy f o l d e d l i f t handle by p u l l i n g handle o u t of stowage d e t e n t and down t o ' l o c k e d position g. Rotate antenna t o h o r i z o n t a l p o s i t i o n and c a r r y t h e antenna t o t h e deployment s i t e by t h e . shimmy b a r (NOTE: The s i t e t o be used should provide a c l e a r view of Earth and b e approximately 20 f e e t from t h e MESA). h. Place - t h e antenna down with t h e bottom antenna handle r e s t i n g . . on t h e s u r f a c e and t h e orientat i o n arrow on top cap pointing , t o Earth. , When CDR moves i n t o SC f i e l d of view, change SC frame r a t e t o 6/sec �CDR - Remove t o p cap: a. b. c. Release each of t h e t h r e e l e g clamps by r o t a t i n g them out and down Depress t h e t h r e e l e g t i p s and push them r a d i a l l y outward t o f r e e t h e antenna t o p cap Discard metal t o p cap and foam piece i n a r e a away from t h e LM Raise antenna mast : While holding t h e antenna vert i c a l , grasp antenna horn t o p p l a t e and r a i s e t h e first s e c t i o n of t h e antenna feed support. (insure t h e f i r s t s e c t i o n only i s deploying by applying a 2-finger pressure on o u t e r mast section. The outer s e c t i o n has orange stripes. ) Do not touch h e l i x eleCAUTION: ----ment when extending feed assembly .b. Check f i r s t s e c t i o n f u l l y deployed and locked i n detent c. Extend t h e second antenna feed s u p p o r t , s e c t i o n i n t h e same manner a s t h e f i r s t . Check t h e second s e c t i o n f u l l y extended and locked i n detent. a. Deploy t r i p o d : a. b. Extend antenna l e g s by placing 2 f i n g e r s about t h e l e g s e c t i o n and applying f o r c e against loops on e i t h e r s i d e of l e g . Continue t o extend each l e g s e c t i o n t o t h e proper' l e n g t h , i .e., t h e proper p a i n t r i n g and lock with clamps. Check adequacy of each l e g lock Check antenna point toward e a r t h by arrow on r i b programmer IMP - �IMP - CDR - Move around t o t h e r i g h t i n t o t h e antenna l i f t i n g position by t h e shimmy bar P u l l each of t h r e e Velcro l e g retension s t r a p s and l e t the l e g s f a l l outward t o a horizontal position on t h e surface Remove thermal covering from antenna and discard away from LM L i f t t h e antenna from t h e surface using both hands on t h e shi,pmy bar u n t i l t h e antenna i s high enough t o permit t h e crewmember t o . g r a s p the lift handle While holding t h e antenna a l o f t with one hand, grasp l i f t handle with other hand L i f t t h e antenna t o t h e high detent position Check each l e g locked securely i n detent by holding the antenna a l o f t with one hand,and pushing outboard on the l e g s individually Set antenna on surface Release p u l l pin fastener a t base of shimmy bar. P u l l deployment bar down and away from antenna Discard bar i n t h e area away from the Firmly implant each l e g i n t o surface ' Open antenna r e f l e c t o r : a, b. c. d. e. Remove r i b t i p protector and allow it t o s l i d e down antenna l e g t o surface Uncoil antenna r e f l e c t o r r e l e a s e cable from around antenna. Hold cable t a u t and i n s t r a i g h t l i n e t o plunger Remove release t r i g g e r guard pin and discard i n area away from IM Graps an antenna l e g with f r e e hand and position s e l f a t arms length from l e g With head down, squeeze release t r i g g e r t o deploy antenna dish. �CDR - IMF - Attach antenna cable: Walk t o f r o n t of MESA, a d j u s t MESA i f necessary P u l l Velcro s t r a p s t o f r e e l e f t s i d e of thermal blanket Unfold lef't s i d e of blanket t o permit easy access t o cable Release antenna cable connector by p u l l i n g Velcro t a b and snap f r e e Grasp cable connector and pass t h e connector under t h e MESA support s t r a p With cable connector i n hand, walk t o t h e lef't of t h e antenna Walk p a s t t h e antenna and deploy t h e cable completely ( u n t i l black and white s t r i p e d section visible ) Walk t o antenna ,Connect antenna cable by mating t h e two connector p a r t s t u r n i n g t h e outer p a r t clockwise a s viewed from cable end Change SC FR t o l / s e c - Rough a l i g n antenna: a. b. c. d. e. Move around antenna l e g t o rough antenna alignment p o s i t i o n Unstow alignment crank by pushing down and away on crank handle Uncoil crank cable by passing crank wound and behind t h e ant enna base Rough a l i g n antenna i n p i t c h (CCW r o t a t i o n of t h e handle p i t c h e s t h e antenna down) Rough align'antenna i n azimuth. Pull antenna crank out from housing then r o t a t e handcrank t o change antenna azimuth Change SC f i l m magazine when necessary �Fine a l i g n antenna: a. b. c . Press each l e g i n t o surface Check antenna alignment by s i g h t i n g along antenna mast and using o p t i c a l alignment s i g h t Fine a l i g n antenna, a s required, by using remote c o n t r o l crankhandle "in" f o r p i t c h and "out" f o r azimuth Rest-check communications and EMU systems. Take one photo of antenna Switch t o e r e c t a b l e antennaS-band s e l e c t o r t o "Lunar stay" (FM, Mode 10) Perform communications check. Check s i g n a l s t r e n g t h indication > 1.0. Verify voice and telemetry with MSFN. Check LM and EMU systems. Determine "GO" f o r EVA Refer t o t h e Nominal EVA procedures, Section 3 . 5 , f o r t h e LMP I n i t i a l EVA procedures. �4.2 Contingent EVA 1 - Minimum Time, One Man 4.2.1 Description and Rationale For various reasons, on the first lunar landing mission only a very limited time may be available to accomplish the,EVA.* For such a situation the choice of objectives are, first, those with the highest priority and, secondly, those which can be accomplished in a Short period of time and do not require the accomplishment of a previous task. The timeline presented here, referred to as the Contingent EVA 1 or Minimum-Time, One-Man EVA, is to optimize the accomplishment of the choice of objectives by providing the maximum data return for the minimum amount of time expended. ( ~ M n A timeline of approximately 49 minutes). There are several other considerations which enter into the selection of the tasks and the procedural detail of the activities for a minimum time EVA. As this will be an unplanned or contingent EVA, it is desirable to have the procedures and sequence of events closely related to the nominal. Either crewman should be equally capable of conducting the desired tasks and contributing to the data returned. And in general, to achieve the maximum diversified data collection, the crewman on the surface will not go into the procedural detail, particularly with verbal descriptions, as he is expected to in the nominal timeline. In this contingent EVA, for the environmental familiarization, the crewman will spend only enough time to assure himself that he can safely proceed with the EVA. After the contingency sample collection he will continue to become more adapted to the new environment as he conducts a limited EVA evaluation. PrimariLy, this EVA evaluation will involve a brief investigation to determine an astronaut's general capabilities or limitations for conducting EVA tasks within the lunar environment. Photographs taken during this evaluation will be a postflight aid to the crewman's recall and the documentation of this activity. A limited LM inspection, with very brief comments and several documentary photographs, can be conducted for the forward half of the spacecraft within a few minutes. To conclude the surface activity the crewman will take a photographic panorama and possibly a few additional photographs of documentary value. In conclusion it should be mentioned that the crewman's surface activity will be confined to an area where he can be constantly monitored by and in communications with the crewman inside the LM. Practically all of the activity can be documented with the sequence camera, and, if the communications capability exists, with the TV. Also, there should be sufficient time and activity for a thorough PLSS analysis. The final Flight Mission Rules for Apollo 11 wil1,govern the selection of the crewman to egress and the EVA he will accomplish. . . ' 86 �4.2.2 T I M E SCALE q C O W N011nr D HODUU ( . .-. E H I LllL SUMMARY TIMELINE CONTINGENT EVA I I0 . ACTIVITY C S M l l M COMM I MCC-H ACTIVlTV I P A R A T C S YUOM UOCKS W S T N l T V t CWRDIMTED TASKS I I. F I ~ LVRE-LVA OI(MTIDUS #DEPRESS FROM 3.) PSI b SEQlENX CALTRA C M R A Q ~ C W E M A C E b FRAME W ~ c w r n ~ c r C . INITIAL N A tcouu T V COVERAGE 1FRAYVYC I1 MINIMUM TIME, ONE MAN COMMANDER ACllVlTY cnrcr ORELEASE Y Y I 0.LRFORU C l U L SYSlLYS CHECKS I 12 F R A U E ~ C . ~DETERUIML GO FOI EVA 24 F R A Y E V I f C 0 1CcoveACE BXgl Y U I C M ~ E OfCTIVATE SEQUENCE CAULMA LM PILOT ACTIVITY IDEPLOV LEE AS SAFETY UOUITOR I l M E SCALE OASCEND LADDER OCOLLECT SAMPLE ODETACH B I C L GISCUD MMDLE OIYCRESS U B I N .+z ORESIXMECI: EMU . OP(IWIDE CHECKLIST ASSISTA*CE I I OP((OT0CRAPWI DA , @ . I +.Y CLU OJETTISOM EPUINENT .SECURE MTCH 1" OREPRESSURIZE CABIN 1-1 GEAR f REV. YLRCH I ITRAMSFER STILL CAYERA 1 0 SURFACE 4.2.2 OR: HENORICKS CH SUMMARY 1IMELINE c o m r l m c r n EVA I (US% Y M . 1969 � Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Title A name given to the resource Saturn V Collection Relation A related resource <a href="http://libarchstor.uah.edu:8081/repositories/2/resources/60" target="_blank" rel="noreferrer noopener">View the Saturn V Collection finding aid in ArchivesSpace</a> Identifier An unambiguous reference to the resource within a given context Saturn V Collection Description An account of the resource <p>The Saturn V was a three-stage launch vehicle and the rocket that put man on the moon. (Detailed information about the Saturn V's three stages may be found<span> </span><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_first_stage.html">here,<span> </span></a><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_second_stage.html">here,<span> </span></a>and<span> </span><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_third_stage.html">here.</a>) Wernher von Braun led the Saturn V team, serving as chief architect for the rocket.</p> <p>Perhaps the Saturn V’s greatest claim to fame is the Apollo Program, specifically Apollo 11. Several manned and unmanned missions that tested the rocket preceded the Apollo 11 launch. Apollo 11 was the United States’ ultimate victory in the space race with the Soviet Union; the spacecraft successfully landed on the moon, and its crew members were the first men in history to set foot on Earth’s rocky satellite.</p> <p>A Saturn V rocket also put Skylab into orbit in 1973. A total of 15 Saturn Vs were built, but only 13 of those were used.</p> Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context spc_stnv_000072 Title A name given to the resource Final Apollo 11 Lunar Surface Operations Plan. Description An account of the resource Prepared by the Lunar Surface Operations Office, Mission Operations Branch, Flight Crew Support Division. Creator An entity primarily responsible for making the resource Wood, William H., Jr. Manned Spacecraft Center (U.S.) Date A point or period of time associated with an event in the lifecycle of the resource 1969-06-27 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Apollo 11 (Spacecraft) Lunar surface vehicles Project Apollo (U.S.) Saturn Project (U.S.) Saturn launch vehicles Space flight to the moon Space vehicles--Moon--Landing Type The nature or genre of the resource Reports Text Source A related resource from which the described resource is derived Saturn V Collection Box 32, Folder 10 University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama Language A language of the resource en Rights Information about rights held in and over the resource This material may be protected under U. S. Copyright Law (Title 17, U.S. Code) which governs the making of photocopies or reproductions of copyrighted materials. You may use the digitized material for private study, scholarship, or research. Though the University of Alabama in Huntsville Archives and Special Collections has physical ownership of the material in its collections, in some cases we may not own the copyright to the material. It is the patron's obligation to determine and satisfy copyright restrictions when publishing or otherwise distributing materials found in our collections. Relation A related resource spc_stnv_000051_000074 https://digitalprojects.uah.edu/files/original/123/8190/r04a05-25.pdf 883d7d5e3561d7b91467af507f729dad Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context Series 04, Subseries A: Huntsville History Title A name given to the resource Series 04, Subseries A: Huntsville History Still Image A static visual representation. Examples include paintings, drawings, graphic designs, plans and maps. Recommended best practice is to assign the type Text to images of textual materials. Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context r04a05-25 Source A related resource from which the described resource is derived Frances Cabaniss Roberts Collection Series 4, Subseries A, Box 5, Folder 25 University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama Title A name given to the resource Finance Report, 1953 Description An account of the resource Utilities and Services Relation A related resource r04a-210924 Creator An entity primarily responsible for making the resource Huntsville (Ala.) Payne, N. M. Date A point or period of time associated with an event in the lifecycle of the resource 1953-09-30 Temporal Coverage Temporal characteristics of the resource. 1950-1959 Subject The topic of the resource Accounts Finances Huntsville (Ala.) Population Taxes Type The nature or genre of the resource Finance reports Language A language of the resource en Rights Information about rights held in and over the resource This material may be protected under U. S. Copyright Law (Title 17, U.S. Code) which governs the making of photocopies or reproductions of copyrighted materials. You may use the digitized material for private study, scholarship, or research. Though the University of Alabama in Huntsville Archives and Special Collections has physical ownership of the material in its collections, in some cases we may not own the copyright to the material. It is the patron's obligation to determine and satisfy copyright restrictions when publishing or otherwise distributing materials found in our collections.