64 20 8242 https://digitalprojects.uah.edu/files/original/20/10312/TEstlabprogrep3_032408084650.pdf f496003799363d256e21e3d2e654e1e7 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 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 <a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_first_stage.html">here, </a><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_second_stage.html">here, </a>and <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. 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. 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. 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 TEstlabprogrep3_032408084650.pdf spc_stnv_000891 Title A name given to the resource "Test Laboratory monthly progress report" July. Description An account of the resource Laboratory monthly progress report for the Saturn 1B program between dates July 1st through July 31st, 1967. Creator An entity primarily responsible for making the resource George C. Marshall Space Flight Center. Test Laboratory. Systems Test Division Date A point or period of time associated with an event in the lifecycle of the resource 1967-08-01 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Saturn project Apollo project Planning Project management NASA space programs Type The nature or genre of the resource Text Progress Reports 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 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_000875_000899 Is Referenced By A related resource that references, cites, or otherwise points to the described resource. http://libarchstor.uah.edu:8081/search?utf8=%E2%9C%93&op%5B%5D=&q%5B%5D=Test+Laboratory+monthly+progress+report+%3A+July+1%2C+1967+through+July+31%2C+1967&limit=&field%5B%5D=&from_year%5B%5D=&to_year%5B%5D=&commit=Search https://digitalprojects.uah.edu/files/original/20/10306/TestlabmonproJUNE_032808134023.pdf 2fdba5e70dcb4e5928125db49fc8a1f2 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 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 <a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_first_stage.html">here, </a><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_second_stage.html">here, </a>and <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. 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. 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. 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 TestlabmonproJUNE_032808134023.pdf spc_stnv_000885 Title A name given to the resource "Test Laboratory monthly progress report" June. Description An account of the resource Laboratory monthly progress report for the Saturn 1B program between dates June 1st through June 31st, 1967. Creator An entity primarily responsible for making the resource George C. Marshall Space Flight Center. Test Laboratory. Systems Test Division Date A point or period of time associated with an event in the lifecycle of the resource 1967-07-01 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Saturn project Apollo project Planning Management NASA space programs Type The nature or genre of the resource Text Progress Reports Source A related resource from which the described resource is derived Saturn V Collection Box 23, Folder 16 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_000875_000899 Is Referenced By A related resource that references, cites, or otherwise points to the described resource. http://libarchstor.uah.edu:8081/repositories/2/archival_objects/17706 https://digitalprojects.uah.edu/files/original/20/10314/TestlabprogrepOCT_041808091527.pdf cfab99d822447c43f71a23a78afb4435 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 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 <a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_first_stage.html">here, </a><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_second_stage.html">here, </a>and <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. 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. 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. 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 TestlabprogrepOCT_041808091527.pdf spc_stnv_000893 Title A name given to the resource "Test Laboratory monthly progress report" October. Description An account of the resource Laboratory monthly progress report for the Saturn 1B program between dates October 1st through October 31st, 1967. Page 17 missing. Creator An entity primarily responsible for making the resource George C. Marshall Space Flight Center. Test Laboratory. Systems Test Division Date A point or period of time associated with an event in the lifecycle of the resource 1967-11-01 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Saturn project Apollo project Planning Project management NASA space programs Type The nature or genre of the resource Text Progress Reports Source A related resource from which the described resource is derived Saturn V Collection Box 23, Folder 63 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_000875_000899 Is Referenced By A related resource that references, cites, or otherwise points to the described resource. http://libarchstor.uah.edu:8081/repositories/2/archival_objects/17753 https://digitalprojects.uah.edu/files/original/20/10305/Testlabmonprogrep_041008104724.pdf c2f16f790474bef09a4a58f7e9c827e4 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 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 <a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_first_stage.html">here, </a><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_second_stage.html">here, </a>and <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. 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. 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. 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 Testlabmonprogrep_041008104724.pdf spc_stnv_000884 Title A name given to the resource "Test Laboratory monthly progress report" September. Description An account of the resource Laboratory monthly progress report for the Saturn 1B program between dates September 1st through September 31st, 1967. Creator An entity primarily responsible for making the resource George C. Marshall Space Flight Center. Test Laboratory. Systems Test Division Date A point or period of time associated with an event in the lifecycle of the resource 1967-10-01 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Saturn project Apollo project Planning Management NASA space programs Type The nature or genre of the resource Text Progress Reports Source A related resource from which the described resource is derived Saturn V Collection Box 23, Folder 51 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_000875_000899 Is Referenced By A related resource that references, cites, or otherwise points to the described resource. http://libarchstor.uah.edu:8081/repositories/2/archival_objects/17741 https://digitalprojects.uah.edu/files/original/20/10309/Testlaboprogfeb1966_083007095938.pdf b2ab6161601a24e5f34a98ce6bc3ad24 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 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 <a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_first_stage.html">here, </a><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_second_stage.html">here, </a>and <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. 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. 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. 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 Testlaboprogfeb1966_083007095938.pdf spc_stnv_000888 Title A name given to the resource "Test Laboratory progress report" Febuary and March. Description An account of the resource Monthly rogress report for the test laboratory regarding the Saturn 1B program between Feburary and March Creator An entity primarily responsible for making the resource Heimburg, Karl L. Date A point or period of time associated with an event in the lifecycle of the resource 1966-03-12 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Saturn project George C. Marshall Space Flight Center. Test Laboratory--Planning Saturn V launch vehicles Saturn 1B launch vehicles Project management Type The nature or genre of the resource Text Progress Reports Source A related resource from which the described resource is derived Saturn V Collection Box 16, Folder 27 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_000875_000899 Is Referenced By A related resource that references, cites, or otherwise points to the described resource. http://libarchstor.uah.edu:8081/repositories/2/archival_objects/17418 https://digitalprojects.uah.edu/files/original/20/10303/teslabprorepmar121966toapr121966_091407131635.pdf d471e036b6f51eb8cb20ce2d2e61969f 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 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 <a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_first_stage.html">here, </a><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_second_stage.html">here, </a>and <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. 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. 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. 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 teslabprorepmar121966toapr121966_091407131635.pdf spc_stnv_000882 Title A name given to the resource "Test Laboratory progress report" March and April. Description An account of the resource Monthly rogress report for the test laboratory regarding the Saturn 1B program between March and April. Creator An entity primarily responsible for making the resource Heimburg, Karl L. Date A point or period of time associated with an event in the lifecycle of the resource 1966-04-12 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Saturn project George C. Marshall Space Flight Center. Test Laboratory Management Saturn 1B launch vehicles Saturn 5 launch vehicles Type The nature or genre of the resource Text Progress Reports Source A related resource from which the described resource is derived Saturn V Collection Box 17, Folder 15 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_000875_000899 Is Referenced By A related resource that references, cites, or otherwise points to the described resource. http://libarchstor.uah.edu:8081/repositories/2/archival_objects/17438 https://digitalprojects.uah.edu/files/original/20/10310/Testlaboprogrepomay121966tojune121966_110107111326.pdf b9e4ef8df735e94174f0da1ac5d8f714 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 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 <a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_first_stage.html">here, </a><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_second_stage.html">here, </a>and <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. 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. 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. 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 Testlaboprogrepomay121966tojune121966_110107111326.pdf spc_stnv_000889 Title A name given to the resource "Test Laboratory progress report" May and June. Description An account of the resource Monthly rogress report for the test laboratory regarding the Saturn 1B program between Feburary and March Creator An entity primarily responsible for making the resource Heimburg, Karl L. Date A point or period of time associated with an event in the lifecycle of the resource 1966-06-12 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Saturn project George C. Marshall Space Flight Center. Test Laboratory--Planning Saturn V launch vehicles Saturn 1B launch vehicles Project management Type The nature or genre of the resource Text Progress Reports Source A related resource from which the described resource is derived Saturn V Collection Box 17, Folder 47 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_000875_000899 Is Referenced By A related resource that references, cites, or otherwise points to the described resource. http://libarchstor.uah.edu:8081/repositories/2/archival_objects/17470 https://digitalprojects.uah.edu/files/original/20/10315/Testoperorgachar_120408111035.pdf af578ee7cde00c08a1a049b2eeda3b55 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 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 <a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_first_stage.html">here, </a><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_second_stage.html">here, </a>and <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. 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. 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. 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 Testoperorgachar_120408111035.pdf spc_stnv_000894 Title A name given to the resource "Test operations:" Organization Chart. Description An account of the resource Organization Chart of the North American Rockwell Test Operations. Creator An entity primarily responsible for making the resource North American Rockwell Corporation. Space Division Date A point or period of time associated with an event in the lifecycle of the resource 1968-08-27 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Saturn project Saturn S-2 stage Organization charts Type The nature or genre of the resource Still Image Organization Charts 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 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_000875_000899 https://digitalprojects.uah.edu/files/original/20/10316/Testprocvalidbycompsimulation_071508150442.pdf 5f2fbaf41fd38a945322f16c3efd6304 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 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 <a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_first_stage.html">here, </a><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_second_stage.html">here, </a>and <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. 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. 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. 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 Testprocvalidbycompsimulation_071508150442.pdf spc_stnv_000895 Title A name given to the resource "Test procedure validation by computer simulation." Description An account of the resource Digital computer simulation of the Saturn I Instrument Unit electrical networks was accomplished using the Discrete Network Simulation programs. The schematics were analyzed and a logic model prepared which consisted of a series of Boolean equations. The test procedures, which are written in the Acceptance, Test, or Launch Language (ATOLL), consist of a sequential set of computer instructions for the RCA llOA checkout computer to control the operation of the electrical networks. The procedures also contain the predicted results for each operation. The driving functions for the simulation of the model are generated from the ATOLL test tape by the Input Generator Program. The time sequenced operation of the networks is indicatedby the output from the simulation program in addition to the number of times each component in the system changes state. The results of the simulation are compared to the test procedure predictions on the ATOLL tape by the Comparator Program and any differences are listed. The Comparator Program also lists any component which did not change state at least once. Creator An entity primarily responsible for making the resource Jaegly, Robert L. Date A point or period of time associated with an event in the lifecycle of the resource 1968-03-27 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Saturn project Electric networks Electric networks Computerized simulation Type The nature or genre of the resource Text Essays Source A related resource from which the described resource is derived Saturn V Collection Box 26, 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_000875_000899 Is Referenced By A related resource that references, cites, or otherwise points to the described resource. http://libarchstor.uah.edu:8081/repositories/2/archival_objects/17857 https://digitalprojects.uah.edu/files/original/132/9408/r10_01-04.pdf 60ef370311cb454524b266fbbc148f2d 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_01-04 Source A related resource from which the described resource is derived Series 10, Box 1, Folder 4 Title A name given to the resource "Testimony of Mrs. George R. Ward," 1883 Relation A related resource r10-211020 https://digitalprojects.uah.edu/files/original/9/1293/spc_dann_000257.mp4 396d544c25625e4db5c0cd0cce8017eb 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 Konrad Dannenberg Collection Identifier An unambiguous reference to the resource within a given context Konrad Dannenberg Collection Relation A related resource <a href="http://libarchstor.uah.edu:8081/repositories/2/resources/99">View the Konrad Dannenberg Collection finding aid on ArchivesSpace</a> 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_dann_000257 MC_43_141 Title A name given to the resource "Thanksgiving 1971, Dallas - mostly Kerry." Description An account of the resource The Dannenbergs visit a friend's house for Thanksgiving. Shown are Kerry and Klaus Dannenberg playing in the front yard of the house where the celebrations are. Fall 1971. Creator An entity primarily responsible for making the resource Dannenberg, Konrad Date A point or period of time associated with an event in the lifecycle of the resource 1971-11 Temporal Coverage Temporal characteristics of the resource. 1970-1979 Subject The topic of the resource Dannenberg, Konrad German Americans Thanksgiving Format The file format, physical medium, or dimensions of the resource 8 mm (photographic film size) Type The nature or genre of the resource Home movies Moving Image Source A related resource from which the described resource is derived Konrad Dannenberg Collection University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, 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. Donated by Klaus Dannenberg. Digitized for the 2019-2020 CLIR Recordings at Risk grant. Language A language of the resource de 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_film_metadata_02 https://digitalprojects.uah.edu/files/original/9/1315/spc_dann_000279.mp4 564c36eb033dea1161e5cdc1652f6762 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 Konrad Dannenberg Collection Identifier An unambiguous reference to the resource within a given context Konrad Dannenberg Collection Relation A related resource <a href="http://libarchstor.uah.edu:8081/repositories/2/resources/99">View the Konrad Dannenberg Collection finding aid on ArchivesSpace</a> 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_dann_000279 MC_43_163 Title A name given to the resource "Thanksgiving 76 at Da's w/ K & B." Description An account of the resource Betty, Klaus, Kerry, and Christie visit Konrad and Ingeborg for Thanksgiving. The four visiting members are shown walking into the house, followed by everyone sitting down for dinner. Monte Sano, Huntsville, Alabama, Fall 1976. Creator An entity primarily responsible for making the resource Dannenberg, Konrad Date A point or period of time associated with an event in the lifecycle of the resource 1976-11 Temporal Coverage Temporal characteristics of the resource. 1970-1979 Subject The topic of the resource Dannenberg, Konrad German Americans Thanksgiving Huntsville (Ala.) Madison County (Ala.) Format The file format, physical medium, or dimensions of the resource 8 mm (photographic film size) Type The nature or genre of the resource Home movies Moving Image Source A related resource from which the described resource is derived Konrad Dannenberg Collection University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, 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. Donated by Klaus Dannenberg. Digitized for the 2019-2020 CLIR Recordings at Risk grant. Language A language of the resource de 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_film_metadata_02 https://digitalprojects.uah.edu/files/original/70/1436/loc_salm_000175.pdf 2de0c920de267f1382e6071b50f0467a 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 M. Louis Salmon Collection Title A name given to the resource M. Louis Salmon Collection Relation A related resource <a href="http://libarchstor.uah.edu:8081/repositories/2/resources/89" target="_blank" rel="noreferrer noopener">View the M. Louis Salmon Collection finding aid in ArchivesSpace</a> 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_salm_000175 Title A name given to the resource "The 'High' Command." Description An account of the resource Salmon is pictured at center. Creator An entity primarily responsible for making the resource Salmon, Maurice Louis Temporal Coverage Temporal characteristics of the resource. 1940-1949 Subject The topic of the resource Salmon, Maurice Louis World War, 1939-1945--Military life World War, 1939-1945--Military personnel Type The nature or genre of the resource Photographs Format The file format, physical medium, or dimensions of the resource Still Image Source A related resource from which the described resource is derived M. Louis Salmon Collection Box 1, Folder 5 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_salm_2019_12 https://digitalprojects.uah.edu/files/original/55/1945/uah_hockey_013.pdf 4091387d25114ddfc77697352ee96949 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 History Collection Identifier An unambiguous reference to the resource within a given context UAH History 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_hockey_013 Title A name given to the resource "The 1988-89 Charger Hockey Team." 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 1988 Temporal Coverage Temporal characteristics of the resource. 1980-1989 Subject The topic of the resource College sports Hockey University of Alabama in Huntsville Huntsville (Ala.) Madison County (Ala.) Type The nature or genre of the resource Fliers (Printed matter) 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. Source A related resource from which the described resource is derived University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama https://digitalprojects.uah.edu/files/original/193/13870/Defense_Billboard_75_001.pdf dca18183f329ac8f2ae3f8d43efcbccf PDF Text Text American Forces Information Service, Department of Defense 601 N. Fairfax Street, Room 312, Alexandria, VA 22314-2007 � 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 Defense Billboard Posters 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 Defense_Billboard_75 Title A name given to the resource "The Answer Is: Wrestling Over the Remote Control.; And the Question: How do potatoes get their exercise?" Alternative Title An alternative name for the resource. The distinction between titles and alternative titles is application-specific. D2.9:D36/2/No.75 Description An account of the resource Potatoes sitting on the couch drinking soda and eating popcorn in front of the TV Creator An entity primarily responsible for making the resource Department of Defense Date A point or period of time associated with an event in the lifecycle of the resource 1994-08-18 Temporal Coverage Temporal characteristics of the resource. 1990-1999 Subject The topic of the resource Department of Defense poster United States--Department of Defense Laziness Potatoes Puns Type The nature or genre of the resource Posters Still Image Source A related resource from which the described resource is derived The University of Alabama in Huntsville M. Louis Salmon Library Defense Billboards Posters Case 1, Drawer 1 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 Defense Billboards https://digitalprojects.uah.edu/files/original/20/1272/spc_stnv_000129.pdf a306bb731d0e758b829ce5bf73574869 PDF Text Text V H E A S T R O D Y N A M I C I S T ' S R O L E V I S - A - V I S T H E SYSTEMS E N G I N E E R bv REYNOLDS DUNCAN, JR. NASA Marshall Space Flight Center Huntsville, Alabama J. Smm U,-,iversitY WB~?'? ~esaarch\'*itUte ;enc;@, HistmY oF Sc Date ---------- Doc.NO. -------I . �Z)EE AS$RODY&MXCIST'S ROLE VIS-A-VIS THE SYSTgMS ENGINEER J. Reynolds Duncan, Jr. Aerospace Engineer NASA-Marshall Space P l i g h t Center W u n t s v i l l e , Alabmna The prablem o f e f f e c t i v e two-way c o m u n i c a t i o n s is t r e a t e d , w i t h emphasis p l a c e d upon t h e compilat i o n a d p r e s e n t a t i o n of astrodynamical d a m f o r w e by t h e systems e n g i n e e r i n t h e p r e l i m i n a r y p h a s e s o f m i s s i o n p l a n n i n g . Such d a t a s h o u l d b e p r e s e n t e d i n a form which is e a s i l y understood and v h i c h c a n n o t b e e a s i l y m i s i n t e r p r e t e d by p e r s o n s w i t h l i t t l e o r no k n o w l e d g e o f a s t r ~ d y ~ r a i c s . Wherever a s t r o d y n a m i c a l p a r a m e t e r s may b p o s e c o n s t r a i n t s upon a m i s s i o n , a c l e a r i n d i c a t i o n s h o u l d be g i v e n o f t h e p o s s i b l e consequences f o r v i o l a t i o n o f t h e s e c o n s t r a i n t s . When a l t e r n a t i v e s a r e a v a i l a b l e , they should be indicated, along w i t h any p e n a l t i e s a s s o c i a t e d w i t h t h e i r u s e . The r e s u l t of t h e astrodynamicist's e f f o r t should be a well-informed systems e n g i n e e r who h a s t h e o v e r a l l p i c t u r e of t h e e f f e c t s o f astrodynamical parameters upon a m i s s i o n and t h u s w i l l be a b l e t o perform meaningful t r a d e o f f s t u d i e s w i t h r e g a r d s t o system d e s i g n a & performance. I. l n t r o d u c t i o n The r o l e a n a s t r o d y n a m i c i s t may p l a y i n a m i s s i o n des.ign s t u d y c a n b e d i v i d e d i n t o two p a r t s : t h a t o f s u p p l y i n g background o r p r e p l a n n i n g i n f o r mation and t h a t o f p r o v i d i n g additions:, u s u a l l y more d e t a i l e d , i n f o r m a t i o n f o r u s e d u r i n g t h e s y s tem and subsystem d e s i g n phase. The t y p e and amount of d a t a s u p p l i e d t o the systems a n a l y s t d u r i n g t h e l a t t e r p h a s e depends t o a l a r g e e x t e n t upon t h e completeness and u s e f u l n e s s o f t h e background i n f o r m a t i o n s u p p l i e d t o him e a r l i e r . The t y p e and method o f p r e s e n t a t i o n of t h i s background i n f o r m a t i o n i s t h e major t o p i c o f d i s c u s s i o n i n t h i s paper. Background i n f o r m a t i o n , a s used h e r e , r e f e r s t o a s t r o d y n a m i c a l d a t a o f a g e n e r a l n a t u r e which may c o n t r o l o r i n f l u e n c e t h e d e s i g n o f systems a n d / o r subsystears. The g e n e r a l f t y o f t h e d a t a i m p l i e s t h a t t h e d a t a may b e used f o r m i s s i o n p l a n n i n g p u r p o s e s on a v a r i e t y o f m i s s i o n s . Of c o u r s e , a l l p o s s i b l e missions? c a n n o t b e covered, b u t by res t r i c t i n g t h e launch, p l a n e t t o b e t h e e a r t h and s p e c i f y i n g a s i n g l e t a r g e t p l a n e t , a manageable gr0.q o f c h a r t s and g r a p h s c o u l d b e g e n e r a t e d c o v e r i n g s u c h p o s s i b i l i t i e s a s d i r e c t and brokenp l a n e t r a n s f e r s f o r a l l r e a l i s t i c launch e n e r g i e s , and a r r i v a l c o n f i g u r a t i o n s v a r y i n g from f l y b y t o low o r b i t a l r e c o n n a i s s a n c e m i s s i o n s . The d a t a p r e s e n t e d s h o u l d i n d i c a t e t h e e f f e c t o r impact o f i m p o r t a n t p a r a m e t e r s upon t h e o v e r a l l c l a s s o f possible missions. The p r e s e n t a t i o n o f t h e d a t a s h o u l d b& a c m p l i s h e d i n s u c h a way a s t o i n d i c a t e p o s s i b l e r a n g e s o f v a l u e s o f t h e parablerere. T h i s i s p r e f e r a b l e t o p r e s e n t i n g sample t r a j e c t o r i e s whieh g i v e only s p e c i f i c values of t h e parameters f o r Whenever t h e v a r i ous s e l e c t e d t r a jsc t o r i e s p o s s i b l e , p a r a m e t e r s which a r e f a m i l i a r t o t h e u s e r s h o u l d be used and when t h e r e i s any p o s s i b i l i t y o f m i s i n t e r p r e t a t i o n o f t h e meaning o f t h e . p a r a m e t e r s , a f u l l e x p l a n a t i o n of t h e i r meaning should accompany t h e c h a r t s o r g r a p h s . Also, t h e v a l a e s o f any c o n s t a n t s used i n the g e n e r a t i o n o f t h e d a t a should b e g i v e n , a l o n g w i t h a n y assumptions which were made which might a f f e c t t h e a c c u r a c y o f t h e d a t a . These may seem t o b e s m a l l p o i n t s , b u t t h e omission o f such items a s t h e s e may c a u s e problems i n t h e p r o p e r u s e and i n t e r p r e t a t i o n o f t h e d a t a . One o f t h e primary c a u s e s of t h e s e omissions i s the f a m i l i a r i t y of the astrodynamicist with the m a t e r i a l h e i s p r e s e n t i n g . Although t h i n g s may b e taken f o r g r a n t e d i n a d i a l o g u e between s p e c i a l i s t s i n t h e same d i s c i p l i n e , making t h e same assumptions when p r e s e n t i n g d a t a t o p e r s o n s i n a n o t h e r f i e l d u s u a l l y r e s u l t s i n a c o m u n i c a t i o n problem. Thus, t h e o b j e c t i v e of t h e a s t r o d y n a m i c i s t s h o u l d b e t o p r e s e n t t o t h e systems e n g i n e e r d a t a which is e a s y t o understand, e a s y t o u s e , and which c a n b e r e g e n e r a t e d w i t h o u t a d d i t i o n a l informa t i o n . To i l l u s t r a t e t h e s e p o i n t s , some g r a p h s w i l l b e p r e s e n t e d which would be used i n a m i s s i o n a n a l y s i s s t u d y o f a n unmanned m i s s i o n t o Mars d u r i n g t h e 1973-74 launch o p p o r t u n i t y . D i s c u s s i o n o f t h e g r a p h s w i l l c e n t e r around t h e t y p e o f i n f o r m a t i o n which should accompany each graph i n o r d e r t o make t h e comunication of t h e information a s e f f e c t i v e a s p o s s i b l e . Space does n o t p e r m i t t h e d i s p l a y o f a more complete s e t ' o f c h a r t s and graphs which might b e used i n such a s t u d y . If. Supplemental I n f o r m a t i o n A graph such a s t h e one shown i n F i g u r e 1 would b e one of t h e f i r s t graphs c o n s u l t e d i n a m i s s i o n a n a l v s i s s t u d y . F i g u r e 1 shows t h e o v e r a l l launch o p p o r t t i n i t y a s d e f i n e d by t h e launch energy, G. From t h i s c h a r t , t h e maximum ranges o f t h e launch d a t e , a r r i v a l d a t e , and time o f f l i g h t c a n b e o b t a i n e d . accompany in^ t h i s graph s h o u l d be i n f o r mation g i v i n g t h e d e f i n i t i o n s o f Type I, 'llype I f , C l a s s 1, and C l a s s 2 t r a j e c t o r i e s a l o n g w i t h a n explana t t o n o f C, a d a n i n d i c a t i o n o f t h e isccur8cy o f t h e d a t a . Also, mention s h o u l d b e made o f any pariameters which may e f f e c t t h e Cg determined launch o p p o r t u n i t y a l o n g w i t h any p o s s i b l e a l t e r n a t i v e a such a s broken-plane t r a n e f s r s . The accompanying i n f o r m a t i o n f o r t h i s f i g u r e might b e p r e s e n t e d a s follows. - Definition of T e r n Type X t r a j e c t o r i e s a r e t h o s e on which t h e spacec r a f t would t r a v e l l e s s t h a n 180"around t h e s u n from t h e time t h e s p a c e c r a f t l e a v e s t h e e a r t h u n t i l i t a r r i v e s a t Mars. Type 11 t r a j e c t o r i e s a r e t h o s e on which t h e s p a c e c r a f t would t r a v e l b e t w e n 180' and 360' around t h e s u n . C l a s s 1 and C l a s s 2 t r a j e e t o r i e s a r e s u b c l a s s e s o f Type X: and 'Sypra I1 and d i f f e r p r i m a r i l y I n t h e f l i g h t times r e q u i r e d , C l a s s 2 t r a j e c t o r i e s having l o n g e r f l i g h t times t h a n C l a s s 1 t r a j e c t o r i e s f o r t h e same launch d a t e and C3. The parameter, C, , comes from t h e e q u a t i o n which g i v e s t h e v e l o c i t y of, a n o b j e c t when t r a v e l i n g �Figure 1 - 1973-74 Launch Opportunity for Mars �250 days LAUNCH Figure 2 - DATE 1973 Type I Launch Opportunity for Mars �o n a c o n i c s e c t i o n . The c o n i c e q u a t i o n f o r t h e v e l o c i t y o f a n o b j e c t is (I) where is the e a r t h ' s gravitational constant, R i s t h e d i s t a n c e from t h e c e n t e r of t h e e a r t h , and a i s a measure o f t h e s i t e o f t h e c o n i c s e c t i o n . Bxpressed i n tenna o f %, Equathon (1) becomes C, is t h e i n j e c t i o n e n e r g y p r o v i d e d t o the spacec r a f t by t h e l a u n c h v e h i c l e and i s e q u a l t o t w i c e t h e t o t a l e n e r g y p e r u n i t miss. A s R becomes v e r y l a r g e , C3 a p p r o a c h e s V?. When t h e s p a c e c r a f t leaves the g r a v i t a t i o n a l influence of the e a r t h , V becomes V-, which i s t h e " v e l o c i t y a t i n f i n i t y " o r t h e "hyperbolic-excess v e l o c i t y . " - I n f o r m a t i o n N e c e s s a r y t o U t i l i z e Graph The C3 l i m i t a t i o n o f t h e l a u n c h v e h i c l e , a s p r o v i d e d by performance s t u d i e s , i s a l l t h a t i s needed. I n f o r m a t i o n O b t a i n a b l e from Graph Ranges o f l a u n c h d a t e s , a r r i v a l d a t e s , and f l i g h t t i m e s a s a f u n c t i o n o f t h e C, l i m i t a t i o n s o f t h e launch v e h i c l e . See F i g u r e 2 f o r a n e n l a r g e d view o f lower v a l u e s o f f o r Type I t r a j e c t o r i e s . See F i g u r e 4 f o r h and a r r i v a l Vm c u r v e s f o r t h e lower e n e r g y Type I t r a n s f e r s , These p a r a m e t e r s may l i m i t t h e s i z e o f t h e C, detgrmined launch opportunity. A d d i t i o n a l C o n s t r a i n t s t o Consider '. ( s e e F i g u r e 4 2 ; a r r i v a l V- ( s e e F i g u r e 4 ) ; ccmmunica t i o n d i s t a n c e r e s t r i c t i o n s ; t r a c k i n g c o n s t r a i n t s ( b o t h e a r t h o r b i t a l and deep s p a c e ) ; o p e r a t i o n a l l i m i t a t i o n s on minimum l e n g t h o f launch period. Assumptions Made/Accuracy o f , Data/Cons t a n t s Used Two-body c o n i c s were used i n t h e computation o f t h e d a t a because t h e c o m p u t a t i o n time r e q u i r e d f o r c o n i c t r a j e c t o r i e s is much l e s s t h a n t h a t r e q u i r e d f o r n u m e r i c a l l y i n t e g r a t e d t r a j e c t o r i e s . Accuracy of the d a t a i s considered adequate f o r mission a n a l y s i s s t u d i e s . u (sun) = .13271544E12, t h e a n a l y t i c ephemeris used t o o b t a i n t h e p l a n e t a r y p o s i t i o n s is d e s c r i b e d i n E n g i n e e r i n g P l a n n i n g Document No. 406, J e t P r o p u l s i o n L a b o r a t o r y , J u l y , 1966. Possible Alternatives It may b e p o s s i b l e t o e x t e n d t h e launch opportuni'ty w i t h t h e u s e o f b r o k e n - p l a n e t r a n s f e r s . T h e s ~a r e t r a j e c t o r i e s on which t h e s p a c e c r a f t t r a v e l s p a r t o f t h e way t o Mars i n one f l i g h t p l a n e a n d , a f t e r a v e l o c i t y c o r r e c t i o n i s made, t r a v e r s e s t h e remaining d i s t a n c e i n a d i f f e r e n t f l i g h t p l a n e . The t o t a l e n e r g y expended (C, + p l a n e change bV + a r r i v a l Vm) i s l e s s f o r t h i s t y p e of t r a n s f e r t h a n f o r e i t h e r a Type I o r Type I1 t r a j e c t o r y when t h e h e l i o c e n t r i c t r a n s f e r angle for a single-plane On t r a n s f e r (Type I o r Type T I ) is n e a r 18$. F i g u r e 1, t h e b r o k e n - p l a n e t r a n s f e r s o f i n t e r e s t would b r i d g e t h e narrow gap between t h e Type Z and Type f I c o n t o u r s . U n a t t r a c t i v e f e a t u r e s o f t h e broken-plane t r a j e c t o r i e s a r e the a d d i t i o n a l o p e r a t i o n a l complexity of t h e m i s s i o n and t h e p o s s i b i l i t y o f l i t t l e o r no r e t u r n o f s c i e n t i f i c i n f o r m a t i o n from t h e v i c i n i t y o f t h e t a r g e t p l a n e t i f t h e plane-change maneuver f a i l s . The s i x subheadings used above r e p r e s e n t a usea b l e and e f f e c t i v e method o f p r e s e n t i n g t h e supplemental i n f o r m a t i o n which should riccompany F i g u r e 1. The ma t e r i a 1 p r e s e n t e d under t h e s e subheadings i s , t o a s t r o d y n a m i c i s t s , of a v e r y f a m i l i a r n a t u r e , and might b e c o n s i d e r e d i n f o r m a t i o n which i s n o t worth i n c l u d i n g s i n c e "everyone knows it." But, a g a i n , it is t h i s f a m i l i a r i t y o f t h e a s t r o d y n a m i c i s t w i t h h i s m a t e r i a l t h a t i s o f t e n t h e c a u s e o f comnunication p r o b l b s . I f t h e above subheadings were used a s a g u i d e o r c h e c k l i s t i n d e t e r m i n i n g whether t h e i n f o r mation accompanying t h e c h a r t s and graphs s u p p l i e d t o t h e systems a n a l y s t i s complete, then t h e p o s s i b i l i t y o f misunderstandings and m i s i n t e r p r e t a t i o n s o f t h e d a t a c o u l d b e reduced. I n t h e d i s c u s s i o n of the ensuing g r a p h s , t h e supplemental i n f o r m a t i o n w i l l n o t b e broken down aad p r e s e n t e d under t h e above subheadings. I n s t e a d , t h e s a l i e n t f e a t u r e s o f t h e graphs w i l l be d i s c u s s e d and t h e terms o r concepts which would b e p r e s e n t e d i n g r e a t e r depth o r d e t a i l i n a n a c t u a l r e p o r t f o r u s e i n m i s s i o n d e s i g n s t u d i e s w i l l b e mentioned b u t not necessarily discussed i n d e t a i l . It s h o u l d b e noted t h a t t h e supplemental i n f o r mation f o r F i g u r e 1, a s p r e s e n t e d above, c o n t a i n s not o n l y Lnformation which may b e u s e f u l f o r t h e c o r r e c t i n t e r p r e t a t i o n o f t h e graph b u t p e r i p h e r a l i n f o r m a t i o n which p r o v i d e s t h e u s e r w i t h a backdrop a g a i n s t which t h e d a t a on t h e graph c a n b e viewed. T h i d p e r m i t s t h e systems a n a l y s t t o i n t e r p r e t t h e d a t a i n a more e f f e c t i v e and meaningful manner. The v a l u e o f a graph such a s F i g u r e 1 i s t h a t i t provides an indication, i n the large, of t h e r e s t r i c t i o n s imposed by t h e launch energy. However, s i n c e t h e g r e a t e s t i n t e r e s t probably c e n t e r s around t h e lower v a l u e s o f C,, graphs such a s t h e one shown i n F i g u r e 2 should a l s o be provided. A complete s e t o f C3 c u r v e s f o r Mars would i n c l u d e seven o f t h e type p r e s e n t e d i n F i g u r e 1 and f o u r t e e n o f t h e t y p e p r e s e n t e d i n F i g u r e 2 (seven graphs o f t h e lower C, v a l u e s f o r t h e Type I t r a n s f e r s p l u s seven graphs o f Also t h e lowet C3 v a l u e s f o r Type I1 t r a j e c t o r i e s ) . i n c l u d e d would be seven graphs showing t h e brokenp l a n e t r a n s f e r s which c o u l d b e used t o b r i d g e t h e energy r i d g e between t h e Type I and Type I1 c o n t o u r s . These t w e n t y - e i g h t graphs would r e p r e s e n t t h e f i f t e e n y e a r p e r i o d r e q u i r e d f o r t h e e a r t h and Mars t o r e t u r n t o a s i m i l a r s p a c e - f i x e d geometry. S i n c e t h e supplemental i n f o m t i o n which should accompany graphs o f t h e type shown i n F i g u r e 2 would b e n e a r l y i d e n t i c a l t o t h a t which i s provided w i t h t h e F i g u r e 1 type o f g r a p h , t h e e n t i r e group o f l a r g e and s m a l l s c a l e C3 c u r v e s f o r both 5 p e I and Type 11 could b e i n c l u d e d under t h e same supplemental informa t i o n s h e e t . The graphs r e p r e s e n t i n g t h e broken-plane t r a n s f e r s would d i s p l a y n o t only t h e launch energy c u r v e s b u t curves r e p r e s e n t i n g t h e AV needed f o r t h e plane-change maneuver i n o r d e r t h a t a proper a s s e s s ment o f t h e energy requirements can b e made. The method o f computation o f t h e AV would need t o b e e x p l a i n e d and a d e t a i l e d i l l u s t r a t i o n o f t h e compari s o n between s i n g l e - p l a n e and broken-plane t r a n s f e r s should a l s o be provided. �8 = DECLINATION OF = INCLINATION OF ORBIT P : Figure 3 - Constraints It would a p p e a r from F i g u r e 1 t h a t a continuous o p p o r t u n i t y t o l a u n c h e x i s t s from a b o u t t h e middle of J u n e , 1973 t o t h e m i d d l e o f assuming t h a t a C, o f 3 0 & / s e t h e maximum launch energy a v a i l a b l e . T h i s month launch o p p o r t u n i t y would indeed b e a v a i l a b l e i f t h e o n l y r e s t r i c t i o n f o r a Mars m i s s i o n was t h e launch energy. However, t h e r e a r e many o t h e r c o n s t r a i n t s which need t o b e c o n s i d e r e d and which impose some r a t h e r s e v e r e r e s t r i c t i o n s on t h i s twenty month launch o p p o r t u n i t y , Consider f i r s t the d e c l i n a t i o n of the outgoing asymptote, F i g u r e 3 shows t h a t i s one of t h e two a n g l e s which d e f i n e t h e d i r e c t i o n o f t h e o u t going a s y m p t o t e ( t h e o t h e r a n g l e b e i n g t h e r i g h t ascension). The o u t g o i n g asymptote i n d i c a t e s t h e d i r e c t i o n t h e s p a c e c r a f t must b e t r a v e l i n g r e l a t i v e t o t h e e a r t h when t h e s p a c e c r a f t l e a v e s t h e e a r t h ' s g r a v i t a t i o n a l i n f l u e n c e . The t h r e e views shown i n F i g u r e 3 i n d i c a t e t h a t any v a l u e o f i may b e used t o obtain the d e s i r e d value of 6 a s long a s i 2 h. T h i s may n o t seem l i k e much o f a r e s t r i c t i o n e x c e p t t h a t t h e v a l u e s o f i which c a n b e o b t a i n e d (assuming t h a t t h e n e a r - e a r t h f l i g h t t a k e s p l a c e i n a pace-fixed p l a n e ) a r e l i m i t e d by t h e l a t i t u d e of t h e launch s i t e and t h e a v a i l a b l e r a n g e o f launch a z i m u t h s . The minimum i n c l i n a t i o n o f t h e p a r k i n g o r b i t which may be o b t a i n e d from a l a u n c h i n g a t Cape Kennedy i s approximately 21;.28', which c a n be a c h i e v e d by l a u n c h i n g due E a s t on a launch azimuth *. - THE ASYMPTOTE E A R T H ' PARKING I HYPElE8OLA VALUES ACHIEVE OF THE i MAY SAME BE 8, USED t i L 81 , R e l a t i o n s h i p o f t h e Parking O r b i t P l a n e t o t h e D e c l i n a t i o n o f t h e Outgoing Asyslptote 111. E v a l u a t i o n o f t h e h and ,V OF MANY TO s OuttOiNG PLANE PERIGEE. NOTE: THE of 90' E a s t of North. The maximum v a l u e o f i i s determined by t h e range s a f e t y r e s t r i c t i o n s a n d / o r t r a c k i n g requirements which r e s t r i c t t h e a v a i l a b l e range o f launch azimuths. Thus, a r a n g e of launch azimuths such a s 70' t o 110' would r e s u l t i n a this maximum a t t a i n a b l e v a l u e of i o f a b o u t 35' would r e s t r i c t t h e u s a b l e v a l u e s of R t o a r a n g e o f +3s0. The r e l a t i o n s h i p between launch azimuth and h w i l l b e d i s c u s s e d i n g r e a t e r d e t a i l i n Section IV. - The h y p e r b o l i c - e x c e s s v e l o c i t y a t a r r i v a l , Vm, is a n o t h e r parameter which r e q u i r e s c o n s i d e r a t i o n i n a m i s s i o n d e s i g n s t u d y . It p r o v i d e s a n i n d i c a t i o n o f t h e minimum amount of veloc'ity which t h e s p a c e c r a f t must l o s e i n o r d e r t o a t t a i n a n o r b i t a b o u t Mare. Of c o u r s e , t h e s m a l l e r t h e d e s i r e d o r b i t a b o u t Mau, (assuming t h e shape of o r b i t , e , i s c o n s t a n t ) t h e g r e a t e r w i l l be t h e impulse o r AV t h a t t h e spacec r a f t w i l l have t o supply. Thus, knowledge of t h e range o f v a l u e s o f Vm would p r o v i d e i n f o r m a t i o n f o r d e t e r m i n i n g t h e s i z e o f r o c k e t motor and amount of f u e l which would be n e c e s s a r y t o a t t a i n an o r b i t a b o u t Mars. Shown i n F i g u r e 4 a r e p l o t s of c o n s t a n t v a l u e s of t h e s e p a r a m e t e r s . The h o r i z o n t a l and v e r t l c a l s c a l e s a r e i d e n t i c a l t o t h o s e used i n F i g u r e 2 s o t h a t t h e e f f e c t af t h e s e two parameters on t h e o v e r a l l Type I launch o p p o r t u n i t y c a n b e e a s i l y e v a l u a t e d . A more e f f e c t i v e way o f p r e s e n t i n g t h e combined e f f e c t of C a r Vm, and h i s t o reproduce t h e c u r v e s o f Vm end h on t r a n s p a r e n c i e s which would o v e r l a y t h e Cg c u r v e s . It can b e s e e n from F i g u r e 4 t h a t f o r Type I �. - . ARRIVAL DATE - .- MAY APR 1974 JAN DEC 1973 NOV 21 ! , , 6 44 JUN 73 1 , , , 16 21 26 , I JUL Figure 4 - , 6 ./ , , , , , , , , , , , 10 15 20 25 30 4 9 AUG SE P LAUNCH DATE I 1 16 21 26 31 5 Curves of b n d Vm f o r the 1973 Q p e I Launch Opportunity for Mars . I 14 i �t r a n s f e r s , t h e e a r l i e s t a r r i v a l d a t e a t %rs would p r o b a b l y b e determined by ,V a n d t h a t e a r l y launch d a t e s a r e r e s t r i c t e d by h . The r e s t r i c t i o n s imposed upon t h e launch o p p o r t u n i t y by V- and 6 a r e more s e v e r e i n o t h e r launch y e a r s than is t h e c a s e i n 1973. For m i s s i o n d e s i g n purposes, c u r v e s o f 6 and ,V would a l s o b e provided f o r use w i t h F i g u r e 1 t y p e g r a p h a s w e l l a s t h e lower enargy Type I1 graphs. A f t e r imposing upon t h e launch o p p o r t u n i t y t h e c o n s t r a i n t s which have thus f a r been d i s c u s s e d , i t m y b e u s e f u l t o i n c l u d e some p i c t u r e s t o i l l u s t r a t e what some o f t h e a v a i l a b l e t r a j e c t o r i e s would look l i k e . Shown i n F i g u r e s 5 and 6 a r e t h r e e o f t h e t r a j e c t o r i e s t h a t c o u l d b e used f o r a 1973 mission. The t r a n s f e r s , and t h e o r b i t s o f e a r t h and Mars, a r e drawn t o s c a l e and a r e viewed from a v a n t a g e p o i n t above t h e North E c l i p t i c P o l e , with t h e s u n a t t h e c e n t e r o f t h e f i g u r e s . An examinat i o n o f t h e t r a j e c t o r i e s would r e v e a l t h a t i n t r a v e r s i n g t h e d i s t a n c e from e a r t h t o Mars, a l l three of the transfers require a heliocentric transf e r a n g l e o f l e s s t h a n 180°, and thus a l l t h r e e a r e Type I t r a n s f e r s . Using t h e p r e v i o u s l y mentioned r e s t r i c t i o n s on A and f& (6 5 +3s0, C j 5 30 & / s e c 2 ) and p l a c i n g a r e s t r i c t i o n upon VW 5 4.0 laa/sec., i t can b e s e e n from F i g u r e s 2 and 4 t h a t t h e t h r e e EARLY LAUMCH - EAALY ARRIVAL t r a j e c t o r i e s f a l l on t h e boundary of t h e launch o p p o r t u n i t y d e f i n e d by t h e upper l i m i t s o f V , :, and $ . The t r a j e c t o r y shown i n P i g u r e 5 is c h a v a c t e r i z e d by v a l u e s o f C3 and which a r e n e a r t h e upper l i m i t s of t h e p e r m i s s i b l e r a n g e s o f t h e s e c o n s t r a i n t s . The two t r a j e c t o r i e s shown i n F i g u r e 6 a r e t h e r e s u l t o f launches which o c c u r l a t e i n t h e launch o p p o r t u n i t y w i t h t h e s h o r t f l i g h t time t r a n s f e r having high ,V and C3 v a l u e s , and t h e long f l i g h t tit r a j e c t o r y r e q u i r i n g t h e maximum a 1 lowa b l e value of &. P l o t s o f t r a j e c t o r i e s such a s t h e s e would be o f v a l u e i n h e l p i n g t o visualize t h e s i m u l a r i t i e s and d i f f e r e n c e s o f t h e t r a n s f e r s which a r e a v a i l a b l e d u r i n g a launch o p p o r t u n i t y . For completeness, a group o f t h e s e p l o t s i n t e n d e d f o r use i n a m i s s i o n d e s i g n s t u d y would a l s o i n c l u d e i l l u s t r a t i o n s o f a few Type I1 t r a n s f e r s a s w e l l a s some broken-plane t r a j e c t o r i e s . IV. Launch Windows Thus f a r , t h e d i s c u s s i o n of m i s s i o n d e s i g n c h a r t s h a s c e n t e r e d around t h e launch o p p o r t u n i t y a s d e f i n e d by 6 , Vm, and C3. T h i s launch o p p o r t u n i t y ( s e e f i g u r e s 2 and 4 ) is a g r i d , w i t h e v e r y p a i r of launch and a r r i v a l d a t e s r e p r e s e n t i n g a s m a l l s q u a r e w i t h i n t h e g r i d . The p e r i o d o f time w i t h i n e a c h o f t h e 24 hour s q u a r e s d u r i n g which a launch c a n o c c u r *D LA'E LATE . A L ~ I C ~ -I L A ' E A R R I V A L LAUNCH E A R L Y ARRIVA! - Pigure 6 Figure S 1973 Type I T r a n s f e r s Drawn to S c a l e �Figure 7 - Launch Azimuth a s a Function o f Launch Time w i t h D e c l i n a t i o n a s t h e Parameter e i s known a s t h e launch window. Note t h a t w i t h i n each launch window t h e v a l u e s o f C,, 6 , and Vm remain r e l a t i v e l y c o n s t a n t . The u s e o f a launch window is d e s i r a b l e s i n c e t h e a l t e r n a t i v e , t h e l a u n c h i n g of a v e h i c l e a t a p r e c i s e t i m e , would n o t p e r m i t a n y unscheduled d e l a y s i n t h e launch prep a r a t i o n s and would n o t a l l o w any h o l d i n g time f o a w a i t improved w e a t h e r c o n d i t i o n s . The d u r a t i o n of t h e launch window depends upon t h e r a n g e of a v a i l a b l e launch a z i m u t h s , t h e l a t i t u d e o f t h e launch s i t e , and t h e d e c l i n a t i o n of t h e o u t g o i n g asymptote, S i n c e t h e v a l u e o f 6 is e s s e n t i a l l y f i x e d , and t h e launch s i t e i s r e l a t i v e l y f i x e d ( a t a l a t i t u d e o f t h e o n l y t h i n g t h a t can b e v a r i e d t o a b o u t 28.28'), a c h i e v e a n extended p e r i o d d u r i n g whi,ch t o launch is t h e launch azimuth. The use o f a v a r i a b l e h u n c h azimuth implies t h e use of a parking o r b i t s o t h a t t h e Eirtel b u r n of t h e o r b i t i n g b o o s t v e h i c l e c a n be properly pos~.rionedw . t t h r e s p e c t t o t h e outgoing asymptote. F i g u r e 7 shows t h e s i z e o f t h e launch window t h a t c a n be o b t a i n e d by v a r y i n g t h e launch me b f s w i t h the a s t e r i s k s ( * I s ) i n d i c a t e t h a t t h e y a r e t o b e r e a d a g a i n s t t h e upper launch t i m e s c a l e , w i t h t h e remaining A ' s t o be r e a d ' a g a i n s t t h e losJer s c a l e . ~h~ e x c e p t i o n i s 6 = 0' which i s r e a d a g a i n s t b o t h launch time s c a l e s . m e d o u b l e v a l u e d n a t u r e of t h e launch time i n d i c a t e s t h a t two s e p a r a t e launch windows may e x i s t w i t h i n one 24 hour p e r i o d . When t h e a v a i l a b l e r a n g e o f launch a z i m u t h s is k n a j n and t h e v a l u e o f 8 is known ( t h i s c a n b e o b t a i n e d from graphs such a s shown i n F i g u r e 4 1 , t h e n t h e l e n g t h o f t h e a v a i l a b l e launch window(s) c a n be o b t a i n e d i n t h e f o l l o w i n g manner. A s s m i ng t h e launch azimuth r e s t r i c t i o n s s t a t e d p r e v i o u s l y (5 110', 2 70') and R h o f +15', f i n d t h e i n t e r s e c t i o n of t h e h = 15'* curve with the horizontal l i n e representing a lqunch azimuth (LAZ) of 70' and n o t e t h e v a l u e of * launch time on t h e s c a l e -1.93 h o u r s . Now move a l o n g t h e 6 = 15'* c u r v e towards t h e upper r i g h t (always move a l o n g t h e c u r v e s o f S i n t h e d i r e c t i o n o f i n c r e a s i n g time on t h e launch time s c a l e ) u n t i l t h e i n t e r s e c t i o n w i t h LAZ = 110' i s reached and n o t e t h i s time on t h e s c a l e below -6.93 h o u r s . Take t h e d i f f e r e n c e between t h e s e two times and f i n d t h a t t h e launch window d u r a t i o n i s f i v e hours. Now t r a c e a l o n g t h e 6 = 15' c u r v e i n a s i m i l a r mannet from LAZ = 70' t o LAZ = 110' and, r e a d i n g a g a i n s t t h e lower launch time s c a l e , t h e d u r a t i o n o f t h e launch window w i l l be found t o b e 22.07 h o u r s minus 17.07 h o u r s , o r f i v e hours. When t h e ran$e of launch azimuths i s s w e t r i c a l a b o u t 90' ( a s i s t h e c a s e w i t h 70°and 110' ) t h e l e n g t h o f t h e two launch wir~dowsw i l l b e i d e n t i c a l . Assume now t h a t t h e launch azimuth r e s t r i c t i o n s a r e 6 8 _< LA2 5 loo0 and t h e v a l u e of 6 is +30°. Tracing along t h e = 30°* c u r v e shows t h a t i t never r e a c h e s t h e r a n g e o f al1o;able launch azimuths and t h u s does n o t prov i d e any launch window. However, t r a c i n g a l o n g t h e = 30' does p r o v i d e a launch window o f 23.77 h o u r s minus 17.50 h o u r s , o r 6.27 h o u r s . The launch times shown on F i g u r e 7 do n o t correspond t o t h e S a s t e r n Standard o r Greenwich Mean times o f launch the time shown on t h e s c a l e s is a r e l a t i v e and n o t a n a b s o l u t e time. S e v e r a l o t h e r s e t s o f c u r v e s , used i n c o n j u n c t i o n w i t h F i g u r e 7 , would be n e c e s s a r y t o supply t h e a c t u a l launch times. The primary r e a sons f o r p r o v i d i n g a f o l d e d launch time w a l e on F i g u r e 7 were t o make i t e a s y t o compute t h e l e n g t h o f time between t h e end o f t h e f i r s t launch window and t h e beginning o f t h e second and t o h e l p r e l a t e t h i s i n f o r m a t i o n t o t h a t on F i g u r e 8. The p r o c e d u r e whieh has been o u t l i n e d above f o r u s i n g F i g u r e 7 i s v a l i d only f o r p o s i t i v e v a l u e s of 6 . When n e g a t i v e v a l u e s o f A a r e ueed i t i s n e c e s s a r y t o move t h e a s t e r i s k s (*IS) from t h e top launch t i m e s c a l e t o * - �thi? bottom launch time s c a l e and then proceed a s before. I n a d d i t i o n t o the d u r a t i o n of t h e launch window, t h e time t h e boost v e h i c l e must spend c o a s t i n g i n t h e parking o r b i t can a l s o be expressed a s a funct i o n of t h e launch azimuth and 6. The use of a c o a s t a r c provides an e f f i c i e n t method f o r t h e prop e r p o s i t i o n i n g of t h e f i n a l burn a r c of t h e boost vehicle t h i s is . t h e burn which removes t h e spacec r a f t from i t s e a r t h parking o r b i t and p l a c e s it o n t o t h e d e s i r e d i n t e r p l a n e t a r y t r a j e c t o r y . Figure 8 and Figure 9 provide a means f o r determining what t h e l e n g t h o f t h e c o a s t time ( o r c o a s t a r c ) must be i n o r d e r t o a c h i e v e t h e proper e a r t h d e p a r t u r e geometry. The i n t e r p r e t a t i o n of Figure 8 i s accomp l i s h e d i n a manner very s i m i l a r t o t h a t used i n Figure 7. Knowing t h e v a l u e of fi needed and t h e range of launch azimuths which can b e used, t h e range of c o a s t a r c s ( c o a s t times) which a r e required can be found on t h e s c a l e s a c r o s s t h e bottom o f t h e graph. The a s t e r i s k s (*'s) have t h e same meaning on Figure 8 a s they d i d on F i g u r e 7 , including t h e switching of s c a l e s f o r n e g a t i v e values o f h . The primary d i f f e r e n c e i n t h e i n t e r p r e t a t i o n of Figure 8 a s opposed t o Figure 7 is t h a t t h e s c a l e s f o r t h e c o a s t time and c o a s t a r c on Figure 8 a r e a b s o l u t e , and t h e r e f o r e i n d i v i d u a l values of c o a s t time (coast a r c ) can be read from t h e graph (on Figure 7 i t was only p o s s i b l e t o read time spans, a s t h e i n d i v i d u a l times on t h e graph were r e l a t i v e ) . For example, assuming a launch azimuth range o f 70' 5 LAZ _< 110' and a 6 of +IS', i t can be seen from Figure 8 t h a t t h e c o a s t a r c - r e q u i r e d f o r one launch window ranges - " from about 85' t o 150°, while a range £ran a b o u t 210' t o 275' is necessary f o r the o t h e r launch window. Since t h e values of t h e c o a s t s r c a r e a b s o l u t e , then i t can a l s o be s a i d t h a t i f a launch azimuth of 70' i s used t o achieve a 6 o f +15', it would be necessary f o r t h e l e n g t h o f t h e earth o r b i t a l c o a s t i n g a r c to* be e i t h e r 1 5 6 o r 275'. *By using Figures 7-and 8 t o g e t h e r , t h e behavior of t h e c o a s t a r c a c r o s s t h e launch wtn%ow(s) can be observed. From t h e above example i t i s h n n n t b d t t h e c o a s t a r c s f o r t h e two launch windavs r a n g e To determine from 85O t o 150' and 210' t o 275'. which is t h e i n i t i a l and which L s t h e f i n a l v a l u e of the c o a s t a r c s it i s necessary to r e f e r back t o Figure 7. Using Figure 7, t r a c e a l o n g t h e curves = +15' i n t h e sense of i n c r e a s i n g launch time. of Notice t h a t both launch windows open using a launch azimuth o f 60' and both c l o s e , f i v e hours l a t e r , with a launch azimuth o f 118. Now, using F i g u r e 8 , t r a c e along t h e 6 = +15' curves and n o t e t h a t t h e only way t h e behavior of t h e launch a z i m t h , a s noted on Figure 7, can be d u p l i c a t e d , i s t o t r a c e along t h e curves o f d e c l i n a t i o n from r i g h t t o l e f t . This method o f nro\reprent alpng t h e l i n e s of c o n s t a n t -%a -&be d e c l i n a t i o n , always moving t o t h e c o r r e c t procedure f o r u t i l i z i n g Figure 8, i.e., within a launch window, a s t h e launch t i m e i n c r e a s e s , t h e c o a s t time (coast a r c ) decreases. 2he ranges of c o a s t a r c s (and c o a s t times) obtained from F i g u r e 8 can be matched t o t h e launch windows o b t a i n e d from Figure 7 by combining t h e values from t h e a s t e r i s k (*) s c a l e s t o d e f i n e one launch window and combining t h e values from t h e unmarked s c a l e s to form t h e o t h e r launch window. ' K e r e f o r e froan the range LAUNCH AZIMUTH (dep) COAST TIME (rnlnl Figure 8 - Launch Azimuth a s a Function of Coast Arc and Coast Time with Declination a s t h e Paradleter �o f launch azimuths and t h e v a l u e o f b used i n t h e example above, t h e following information i s obtaina b l e front Figures 7 and 8. Two launch witidows a r e a v a i l a b l e , both o f f i v e hours d u r a t i o n . The f g r s t launch w i d o w opens w i t h a launch azimuth o f 7@ and a c o a s t time o f d m u t 37 minutes. As t h e launch tZme *ncreases, the launch azimuth slowly i n c r e a s e s and t h e c o a s t time slowly d e c r e a s e s u n t i l , a t t h e end of t h e f i r s t window, t h e launch a z i m t % has reached 110' and t h e c o a s t time h a s d e c l i n e d to about 21 d n u t e s . About 1 0 hours l a t e r the second launch window opens w i t h a launch azimuth of 70' and a c o a s t time o f about 67 minutes. Acxoss t h e window, t h e launch azimuth and c o a s t time v a r y slowly, a s b e f o r e , u n t i l a t t h e end o f tIy f i v e hour wendow, t h e launch azimuth a t t a i n s 110' and t h e c o a s t t i m e reaches 51 minutes. I n a d d i t i o n t o t h e launch azimuth and 6, t h e c o a s t a r c 19 a l s o a f u n c t i o n of such t h i n g s a s t h e parking o r b i t r a d i u s , t h e i n j e c t i o n energy (C,) t h e t&e aneomely of' t h e iWje.ction. i t i W a t h e escape hyperb o l a , t h e l e n g t h o f t h e f i r s t and second burn a r c s of t h e b o o s t v e h i c l e , t h e r a d i u s o f c l o s e approach of t h e escape hypefbola, and t h e l a t i t u d e of t h e launch s i t e . Constant values were assumed f o r a l l of t h e s e parameters and t h e values t h a t were used should c e r t a i n l y b e included w i t h thh supplemental information provided w i t h t h e graph. It may n o t be necessary t o i n c l u d e a f u l l e x p l a n a t i o n of t h e meani n g of t h e s e parameters, b u t t h e aystems a n a l y s t should be provided w i t h t h e knowledge t h a t assumpt i o n s were made and should be given t h e values of . t h e c o n s t a n t s t h a t were used. The values o f t h e c o n s t a n t s used i n t h e g e n e r a t i o n o f t h e d a t a o f Figure 8 a r e , i n t h e o r d e r given above and beginning = 6583 km (a 100 w i t h t h e parking o r b i t r a d i u s : 12.125 n a u t i c a l m i l e a l t i t u d e parking o r b i t ) ; C, k d ? s e c 2 ; u = 16.2'; 4 = 20.47'~ I)1 = 29.0'; RCA = 6583 km; m = 28.28'. Since Pigure 8 could be expected t o be used w i t h a wide range of Cj '8, and a change i n t h e C3 does a f f e c t t h e v a l u e of t h e c o a s t time ( c o a s t a r c ) , t h e e f f e c t o f a v a r i a t i o n i n C, upon t h e launch window w i l l be discussed b r i e f l y . A s f o r t h e e f f e c t of t h e o t h e r parameters upon t h e c o a s t time, s u f f i c e i t t o say t h a t i f a launch i s made from Cape Kennedy w i t h a S a t u r n V c l a s s v e h i c l e , t h e information obtained from Figure 8 would be completely adequate f o r use i n mission design s t u d i e s . I f t h e launch window information obtained from Figure 8 i s a s s o c i a t e d w i t h a n i n t e r p l a n e t a r y t r a j e c t o r y which r e q u i r e s a n i n j e c t i o n energy (C,) t h a t i s d i f f e r e n t from 12 .I25 I& /sec2, then a c o r r e c t i o n should be made t o t h e c o a s t times ( c o a s t a r c s ) provided by Figure 8. Figure 9 shows t h e amount of t h e c o a s t time c o r r e c t i o n a s a f u n c t i o n of Simply combine t h e a p p r o p r i a t e c o a s t time C,. c o r r e c t i o n from Figure 9 w i t h t h e values of t h e c o a s t time obtained from Figure 6. + COAST TIME ( m i n l , % - To complete t h e supplemental informatioh which would accompany Figures 7 and 8 i n a mission design document, mention should be made of t h e use of "dog- leg" maneuvers which could be used t o extend t h e launch window. Of course, t h e p e n a l t i e s i n c u r r e d from t h e use of a "dog-leg" maneuver should a l s o be d i s c u s s e d . A s mentioned previously, i f t h e s i x subheadings l i s t e d under S e c t i o n I1 a r e used a s a c h e c k l i s t i n t h e p r e p a r a t i o n of t h e supplemental information which should accompany each c h a r t o r graph, then t h e l i k e l i h o o d of misunderstandings and m i s i n t e r p r e t a t i o n s can be reduced, and t h e systems engineer can u t i l i z e t h e d a t a with f u l l knowledge of t h e options which a r e a v a i l a b l e t o him. Figure 9 .. . V. - Parking-Orbit Coast Time Correction a s a Function of C, - < ~t eal l i t e O r b i t a l Considera t i o n s The f i n a l phase t o be considered i n a mission design study i s t h e a r r i v a l of t h e s p a c e c r a f t a t t h e trjirget p l a n e t . The a s trodynamica 1 d a t a supplied t o the' systems a n a l y s t i n support of t M s phase of t h e study i s c h i e f l y concerned with t h e r e p r e s e n t s t i o n and c l a s s i f i c a t i o n of t h e c h a r a c t e r i s t i c s o f a l l a v a i l a b l e o r b i t s about Mars, and t h e method by which these o r b i t s can be a t t a i n e d . It i s n o t f e a s i b l e , w i t h i n t h e l i m i t e d space a v a i l a b l e i n t h i s paper, t o p r e s e n t and d i s c e s s the c h a r t s and graphs which would b e used t o c l a s s i f y and l o c a t e s p e c i f i c o r b i t s of i n t e r e s t . The d i s c u s s i o n w i l l d e a l p r i marily with the major s c i e n t i f i c and engineering c o n s t r a i n t s which must be considered i n the course of t h e o r b i t s e l e c t i o n process. Since t h e primary reason f o r an o r b i t a l reconnaissance mission t o Mars i s the s c i e n t i f i c invest i g a t i o n of t h e p l a n e t , i t would seem reasonable t o c o n s i d e r f i r s t t h e s c i e n t i f i c c o n s t r a i n t s upon t h e o r b i t . These requirements might i n c l u d e r e s t r i c t i o n s on, o r s p e c i f i c a t i o n s o f , t h e o r b i t ' s s i Z e , shape, i n c l i n a t i o n and o r i e n t a t i o n f o r such purposes a s photography, W photometry, meteorology, f i e l d s and p e r t i c l e s measurements, S-band o c c u l t a t i o n s , magnerometer measurements, o r r e l e a s e of a lander capsule. When a l l of t h e r e s t r i c t i o n s which r e s u l t from experiments such a s these a r e imposed upon t h e o r b i t , t h e r e s u l t i n g number of p o s s i b l e o r b i t s which could be used i s , a t b e s t , s e v e r e l y reduced. Nat, consider t h e engineering c o n s t r a i n t s upon t h e o r b i t . These c o n s t r a i n t s a r e imposed s o t h a t t h e various s p a c e c r a f t systems and subsystems w i l l o p e r a t e e f f e c t i v e l y and e f f i c i e n t l y , and thus permit t h e s c i e n t i f i c i n v e s t i g a t i o n s mentioned above t o proceed normally. The engineering c o n s t r a i n t s may p l a c e requirements on the o r b i t f o r such things a s power generation ( s p a c e c r a f t must remain i n s u n l i g h t �.- p 5 -. a s much a s p o s s i b l e ) , navigation ( s p a c e c r a f t must maintain f i x on n a v i g a t i o n a l s t a r t s ) ) , and commun i c e t i o n s (spacpcraf t must maintain c o n t a c t with e a r t h f o r t h e transmission of d e w ) . I n a d d i t i o n t o these c o n s t r a i n t s t h e l i m i t a t i o n imposed by t h e performance of t h e s p a c e c r a f t retro-propulsion system must be conaiderad. This performance ca2ab i l i t y p l a c e s a lower bound on t h e s i t e and shaoe of t h e o r b i t s which can be a t t a i n e d about Mars. The l i m i t a t i o n s imposed by t h i s c o n s t r a i n t a r e represented on t h e i n t e r p l a n e t a r y launch opportunity c h a r t s by t h e parameter VW (see Figure 4). When a l l o f t h e s c i e n t i f i c and engineering c o n s t r a t n t s which have thus f a r been discussed a r e imposed, i n t o t a l , a s requirements upon t h e o r b i t , t h e number of o r b i t s which can provide t h e d e s i r e d c h a r a c t e r i s t i c s is o f e n zero. Thus, s i n c e i t w i l l very l i k e l y be t h e c a s e t h a t everything which i s required o r d e s i r e d cannot be achieved, i t w i l l be necessary f o r t h e systems a n a l y s t t o perform t r a d e o f f s t u d i e s i h o r d e r t o maximize t h e t o t a l s c i e n t i f i c r e t u r n from t h e mission. The arrtrodpnamicist should t h e r e f o r e supply d a t a which would r e p r e s e n t , i n an e f f e c t i v e manner, t h e impact of each of t h e c o n s t r a i n t s upon t h e s i z e , shape, i n c l i n a t i o n , and o r i e n t a t i o n of t h e a v a i l a b l e o r b i t s , and which would i n d i c a t e t o t h e a n a l y s t t h e a v a i l a b l e ranges of t h e q r b i t a i parameters s o t h a t t h e s t u d i e s can be perfomed i n a n e f f i c i m t and m n i n g f u l manner. , The e f f e c t i v e t r a n s f e r of d a t a from t h e a s t r o dynamicist t o t h e systems engineer can be accomp l i s h e d r a t h e r e a s i l y i f e l i t t l e c a r e i s taken i n t h e p r e p a r a t i o n of t h e supplemenU1 information which should aceompany each of t h e c h a r t s and graphs. The use of a c h e c k l i s t i n t h e p r e p a r a t i o n of t h e supplemental i n f o m t i o n may help t o e l i m i n a t e omissions which may occur because of t h e a s t r u dynamicist's f a m i l i a r i t y w i t h h i s own m a t e r i a l . The o b j e c t i v e of the astrodynamicist should be t o p r e s e n t t o t h e systems engineer material'whicF can be used e s s i l y and e f f e c t i v e l y , and which w i l l cont a i n a l l of t h e supplemental information necessary t o enable t h e system a n a l y s t t o perform meaningful tradeof f s t u d i e s atid make knowledgeable d e c i s i o n s . � 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 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 <a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_first_stage.html">here, </a><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_second_stage.html">here, </a>and <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. 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. 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. 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_000129 Title A name given to the resource "The Astrodynamicist's Role vis-a-vis the Systems Engineer." Alternative Title An alternative name for the resource. The distinction between titles and alternative titles is application-specific. AIAA Paper No. 69-124 Description An account of the resource By J. Reynolds Duncan, Jr., Aerospace Engineer, NASA Marshall Space Flight Center, Huntsville, Alabama. AIAA 7th Aerospace Sciences Meeting, New York City, New York, January 20 - 22, 1969. Creator An entity primarily responsible for making the resource Duncan, J. Reynolds, Jr. George C. Marshall Space Flight Center Date A point or period of time associated with an event in the lifecycle of the resource 1969-01-22 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Astrodynamics Communication of technical information Space flight to Mars Systems engineering 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 30, Folder 14 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_000119_000149 Is Referenced By A related resource that references, cites, or otherwise points to the described resource. http://libarchstor.uah.edu:8081/repositories/2/archival_objects/18064 https://digitalprojects.uah.edu/files/original/76/3327/loc_burw_-145_193.pdf 3262d7c0fd1895d8a235ea8b70201ce7 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 Burwell Family Collection Title A name given to the resource Burwell Family Collection Relation A related resource <a href="http://libarchstor.uah.edu:8081/repositories/2/resources/145" target="_blank" rel="noreferrer noopener">View the Burwell Family Collection finding aid in ArchivesSpace</a> Description An account of the resource <a href="http://libarchstor2.uah.edu/digitalcollections/items/show/3332" target="_blank" rel="noreferrer noopener">View Edwin D. Burwell's World War II service timeline, 1943-1944</a> <a href="http://libarchstor2.uah.edu/digitalcollections/items/show/3333" target="_blank" rel="noreferrer noopener">View Edwin D. Burwell's World War II service timeline, 1944-1945</a> 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. Materials donated and digitized by Dudley Burwell 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_burw_000145_000193 Title A name given to the resource "The Battalions-History of the 1108th Engineer Combat Group". Description An account of the resource This pamphlet was mailed to a Mr. William Rate. It includes photographs of the commanders, a list of "Those Who Are Still There" to chronicle who died overseas and where, and the history of the 1108th Engineer Combat Group. Creator An entity primarily responsible for making the resource Reardon, Mark J., 1957 October 22- Subject The topic of the resource United States. Army. Engineer Combat Group, 1108th World War, 1939-1945 Type The nature or genre of the resource Pamphlets Text Source A related resource from which the described resource is derived Burwell Family 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 loc_burw_2021_02 https://digitalprojects.uah.edu/files/original/125/8480/r04c04-19.pdf edff1690d3e7450bc2f8baafb2fe031b 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 C: Alabama History Title A name given to the resource Series 04, Subseries C: Alabama 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 r04c04-19 Source A related resource from which the described resource is derived Series 4, Subseries C, Box 4, Folder 19 Title A name given to the resource "The Bicentennial of the Constitution" Booklet and Correspondence, 1987 Relation A related resource r04c-211007 https://digitalprojects.uah.edu/files/original/20/1663/Casecomp_091907132002.pdf f753981087c068ed6eccef828f6370da 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 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 <a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_first_stage.html">here, </a><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_second_stage.html">here, </a>and <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. 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. 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. 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 Casecomp.pdf spc_stnv_000190 Title A name given to the resource "The Case for Compatibility." Description An account of the resource "The Case for Compatibility" is a paper by Robert L. Smith, Jr., who worked in Quality and Reliability Assurance Laboratory at George C. Marshall Space Flight Center. The summary states, "Ever since the use of missiles and space launch vehicles began, questions have existed in every program regarding the similarity between upstream (e.g., manufacturing, static firing ) and launch site checkout equipment. Programs have existed which utilized nearly identical equipment for both uses; other programs have existed in which any resemblance of the equipment was probably coincidental. Many factors have entered the final decisions, not the least of which were economic and schedule considerations, and, in some instances, the organizational structure of the developer." Creator An entity primarily responsible for making the resource Smith, Robert L., Jr. Date A point or period of time associated with an event in the lifecycle of the resource 1966-04 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Saturn V Saturn Project (U.S.) Saturn launch vehicles Saturn 5 launch vehicles Spacecraft test equipment Checkout Compatibility Quality assurance--Management Source A related resource from which the described resource is derived Saturn V Collection Box 17, Folder 61 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_000175_000199 Type The nature or genre of the resource Reports Text https://digitalprojects.uah.edu/files/original/20/1665/challchancontrproc_071207105109.pdf 8714b456ba08716cde160e5d12a556fd 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 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 <a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_first_stage.html">here, </a><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_second_stage.html">here, </a>and <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. 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. 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. 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 challchancontrproc.pdf spc_stnv_000192 Title A name given to the resource "The Challenge of Change vs the Control of the Process." Description An account of the resource The introduction states, "This paper is designed to present the Rocketdyne engine program as it applies to the Saturn launch vehicles and will apply to the Apollo program of manned flight to the moon (Fig. 1). The vehicle that will launch this flight is the Saturn V, the largest and most powerful of the Saturn family. This vehicle, 362 feet tall and 33 feet in diameter, will be capable of sending a 45-ton payload to the moon or placing a 120-ton payload in earth orbit. Five F-1 engines power the first stage of the Saturn V; five J-2 engines, the second stage; and one J-2 engine, the third stage. The thrust of the first-stage engines alone will be equivalent to 160 million horsepower. Both of these engines, the F-1 and the J-2, were designed at, and are currently being produced by Rocketdyne." Creator An entity primarily responsible for making the resource Clark, Ross Date A point or period of time associated with an event in the lifecycle of the resource 1964-12-01 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Saturn V Saturn Project (U.S.) Project Apollo (U.S.) Saturn launch vehicles--Design and construction Liquid propellant rockets Liquid propellant rocket engines North American Aviation. Rocketdyne Division Source A related resource from which the described resource is derived Saturn V Collection Box 12, Folder 42 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_000175_000199 Type The nature or genre of the resource Reports Text