Combustion Oscillations in F-1 Engine.
subject: Saturn project
subject: F-1 rocket engine
subject: Liquid propellant rockets
subject: Combustion
description: The set of documents includes an introductory letter written by D. Brainerd Holmes and Tischler's report with the subject "F-1 Combustion Instability Report for Associate Administrator; Period March-April, 1963".
creator: Holmes, D. Brainerd
creator: Tischler, A. O.
source: Saturn V Collection
source: University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama
date: 1963-05-17
rights: 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: spc_stnv_000200_000224
language: en
type: Text
type: Progress Reports

"Digest of FY-63 funded advanced studies : July 1966."
subject: Saturn project
subject: Astronautics--United States
subject: George C. Marshall Space Flight Center. Research Program Office
description: This publication is, one of a planned series to summarize the advanced study program for each fiscal year beginning with FY-61. A separate report will cover the study program for each fiscal year. The purpose of these documents is to provide historical reference information which should be helpful in planning future study programs. The FY-63 funded studies are covered in this document. These investigations are covered under three categories: Launch Vehicle and Supporting Studies; Orbital and Lunar Studies; and Planetary Studies. The information presented on each study includes a brief description of the objective and results and pertinent contract data. In order to keep this report small and easy to use, no attempt was made to include conclusions based on the study results; however, the final reports documenting the investigations are referenced. If these reports are needed for permanent retention and are not available from the Technical Supervisor or the MSFC Library (MS-IPL), submit requests for the documents to the Scientific and Technical Information Facility, Attention: NASA Representative, P. O. Box 33, College Park, Maryland 20740.
creator: Payne, William R.
source: Saturn V Collection
source: Box 17, 72
source: University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama
date: 1966-07-01
rights: 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: spc_stnv_000225_000249
language: en
type: Text
type: Essay

"Digest of FY-62 Funded Advanced Studies : July 1966."
subject: Saturn project
subject: Astronautics--United States
subject: George C. Marshall Space Flight Center. Research Program Office
description: This publication is one of a planned series to summarize the MSFC advanced study program for each fiscal year beginning with FY-61. A separate report will cover the study program for each fiscal year. The purpose of these documents is to provide historical reference information which should be helpful in planning future study programs. The FY-62 funded studies are covered in this document. These investigations are covered under two major categories: Launch Vehicle Studies; and Lunar, Orbital, and Planetary Studies. The information presented on each study includes a brief description of the objectives and results and pertinent contract data. In order to keep this report small and easy to use, no attempt was made to include conclusions based on the study results ; however,the final reports documenting the investigations are referenced. If these reports are needed for permanent retention and are not available from the MSFC Library (MS-IPL), submit requests for the documents to the Scientific and Technical Information Facility, Attention: NASA Representative, P.0. Box 33, College Park, Maryland 20740.
creator: Payne, William R.
source: Saturn V Collection
source: Box 17, Folder 71
source: University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama
date: 1966-07-01
rights: 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: spc_stnv_000225_000249
language: en
type: Text
type: Essay

Differences of configuration in successive Saturn IB and Saturn V vehicles- case 330.
subject: Saturn project
subject: Saturn launch vehicles.
subject: Launch vehicle configurations
subject: Saturn 1B launch vehicles
subject: Saturn 5 launch vehicles
description: Includes memorandum for file. Configuration matrices reflecting present program status of differences in Saturn IB and Saturn V flight hardware on a mission to mission basis have been prepared. The attached matrices are arranged to show differences in major subsystems (Structures, Propulsion, Instrumentation and Range Safety, and Electrical) for each stage. The reason for the configuration difference and the mission effectivity are included.; DMD, 2031-SGE-eas, GRH; Includes "Recommendation for announcement and distribution of Bellcomm Report".
creator: Bellcomm, Inc.
source: Saturn V Collection
source: Box 15, Folder 34
source: University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama
date: 1965-11-10
rights: 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: spc_stnv_000225_000249
language: en
type: Text
type: Memorandums

"Development Status for Arc Guidance, Weld Observation Systems, and a Review of Process Control Parameters."
subject: Saturn project
subject: Electric welding
subject: Saturn launch vehicles
subject: Saturn S-1C stage
description: Letter to David L. Christiensen from W. A. Wall, enclosing requested documents.
creator: Wall, W. A.
source: Saturn V Collection
source: Box 12, Folder 19
source: University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama
date: 1964-09-01
rights: 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: spc_stnv_000225_000249
language: en
type: Text
type: Correspondence

"The Development of Servovalves with Improved Reliability for Space Vehicles."
subject: Saturn project
subject: Automatic control valves
subject: Space vehicles
subject: Servomechanisms
description: Considerations for improvement in the reliability of the Saturn engine gimbal servosystems are briefly covered. The Saturn I servovalves operate with increased electrical input power. The Saturn V vehicle stages will use mechanical feedback actuators with increased electrical input power, larger orifices and nozzle sizes, larger torque motor wire size, and greater spool driving forces.
creator: Kalange, M. A.
creator: Pollock, W. H., Jr.
creator: Thayer, W. J.
source: Saturn V Collection
source: University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama
date: 1964-09-14
rights: 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: spc_stnv_000225_000249
language: en
type: Text
type: Essays

"Development of the Saturn S-IV and S-IVB Liquid Hydrogen Tank Internal Insulation."
subject: Saturn project
subject: Liquid hydrogen
subject: Liquid oxygen
subject: Liquid propellant rockets
subject: Insulation
description: In April of 1960 the Douglas Aircraft Company was awarded a contract to develop the second and uppermost stage for the Saturn I space booster. In order to realize the high specific impulse available, this stage, called the S-IV, was to utilize liquid hydrogen and liquid oxygen as the propellants. After burn-out of the first stage, the S-IV Stage was to ignite its engines at an altitude of approximately 200,000 feet, burn for approximately 8 minutes, and inject a 20,000 lb spacecraft into a low earth orbit. This program represented Douglas's first major endeavor with liquid hydrogen. It was necessary to develop an insulation for the S-IV Stage that was capable of withstanding the thermal shock associated with loading, could provide adequate insulative properties to limit the flow of heat into the hydrogen, and was of minimum weight. This latter fact cannot be over emphasized because every extra pound of insulation is one less pound of available payload weight.
creator: Dearing, D. L.
creator: North American Aviation. Space and Information Systems Division
creator: George C. Marshall Space Flight Center. Test Laboratory
source: Saturn V Collection
source: Box 14, Folder 50
source: University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama
date: 1965-08-23
rights: 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: spc_stnv_000225_000249
language: en
type: Text
type: Essays

Development of LOX/RP-1 engines for Saturn/Apollo launch vehicles.
subject: Saturn project
subject: Liquid oxygen
subject: Liquid propellant rockets
subject: RP-1 rocket propellant
subject: Saturn launch vehicles
subject: Apollo project
description: The development of liquid rocket engines follow similar patterns regardless of engine size. During the development of the H-1 and F-1 engines, may problems were encountered. Mehtods of solving the combustion instability problem are discussed.; AIAA 4th Propulsion Joint Specialist Conference, Cleveland, Ohio, June 10-14, 1968.; Also available on NASA Technical Reports Server (NTRS) as unclassified. Can be ordered. Also on AIAA.
creator: Bostwick, Leonard C.
source: Saturn V Collection
source: Box 27, Folder 11
source: University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama
date: 1968-06-14
rights: 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: spc_stnv_000225_000249
language: en
type: Text
type: Essays

"Development of LOX/RP-1 Engines for Saturn/Apollo Launch Vehicles."
subject: Saturn project
subject: Liquid oxygen
subject: Liquid propellant rockets
subject: RP-1 rocket propellant
subject: Saturn launch vehicles
description: The development of liquid rocket engines follow similar patterns regardless of engine size. During the development of the H-1 and F-1 engines, many problems were encountered. Methods of solving the combustion instability problem are discussed. A description is given of the major components of each engine, outlining their unique features. The requirements for an insulation cocoon are discussed. Problems associated with materials substitution are provided; also highlighted is the fact that problems occur after engine deliveries and require continued development support. Safety features incorporated on the engines are mentioned. Solution to problems encountered in flight are discussed. Upratings of both engines systems are presented graphically.; On the NASA Technical Reports Server (NTRS) unclassified. Can also be found on AIAA.
creator: Bostwick, Leonard C.
source: Saturn V Collection
source: Box 27, Folder 11
source: University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama
date: 1968-06-14
rights: 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: spc_stnv_000225_000249
language: en
type: Text
type: Essays

"Development of LOX-Hydrogen Engines for the Saturn Apollo Launch Vehicles."
subject: Saturn project
subject: Saturn launch vehicles.
subject: Liquid propellant rockets
description: During the development of the RL-10 and J-2 engines, many problems were encountered. Solutions to the significant problems are contained. A description of these LOX-Hydrogen engines, outlining the unique features of each will be given. Performance parameters for both engine systems are tabulated. Specific applications to various stages are shown.
creator: Burks, A. J.
source: Saturn V Collection
source: Box 27, Folder 7
source: University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama
date: 1968-06-10
rights: 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: spc_stnv_000225_000249
language: en
type: Text
type: Essays
identifier: Development of LOX-Hydrogen engines_041207113632.pdf

"Development of Separable Connectors for the Saturn S-IV Stage."
subject: Saturn project
subject: Fluid transmission lines
subject: Saturn launch vehicles
subject: Connectors
description: The purpose of this paper is to present information, in the area of separable connectors as they pertain to the Saturn S-IV Program.
creator: Wilson, E. L.
creator: Coronado, R. J.
creator: Pierson, D. D.
source: Saturn V Collection
source: Box 15, Folder 45
source: University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama
date: 1966-01-01
rights: 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: spc_stnv_000225_000249
language: en
type: Text
type: Essays

"Development of the NASA/Grumman Lunar Module."
subject: Saturn project
subject: Lunar surface vehicles
subject: Saturn launch vehicles
description: Paper regarding the actions and achievement of the Grumman Aerospace Corporation.
creator: Grumman Aerospace Corporation
source: Saturn V Collection
source: Box 31, Folder 44
source: University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama
date: 1969-06-01
rights: 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: spc_stnv_000225_000249
language: en
type: Text
type: Essays

"Development Effort to Achieve Reliability."
subject: Saturn project
subject: Reliability (Engineering)
subject: Space vehicles--Reliability.
subject: Systems engineering.
subject: Spacecraft reliability
description: Presented at the 6th West Coast Reliability Symposium, University of California at Los Angeles, Los Angeles, California, 20 February 1965.The development of a large liquid rocket engine can represent the expenditure of several hundred million dollars of effort. Before 30 percent of the contracted development funds have been expended, however, the engine will probably have operated for the mission duration. The capability to operate at least one successful test early in a development program is evidence of achieving a minimal reliability level, but the major objective of the development program is producing a design which performs reliably. A rocket engine reliability prediction must view reliability as a dynamic concept, constantly being altered by development effort.
creator: Clark, G. M.
creator: Haigler, K. B.
source: Saturn V Collection
source: Box 13, Folder 9
source: University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama
date: 1965-02-20
rights: 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: spc_stnv_000225_000249
language: en
type: Text
type: Essays

"Development and Utilization of Computer and Test Programs for Checkout of Space Vehicles."
subject: Saturn project
subject: Computer systems design
subject: Automatic test equipment
subject: Saturn launch vehicles.
subject: Saturn launch vehicles
description: A computer system was designed to allow test engineers to progressively employ automation in the checkout of the Uprated Saturn I and Saturn V space vehicle programs and still allow manual control of the checkout process. A two-computer system was selected by National Aeronautics and Space Administration, and the International Business Machines Corporation was chosen to provide the programming engineering necessary to implement these objectives. Space vehicle checkout, prior to launch, may be characterized by controlling, monitoring, and testing the vehicle and its subsystems through the use of ground support equipment (GSE).; IBM Huntsville Library.; Presented at AIAA Conference, XVIIth International Astronautical Congress, Madrid, Spain, October 10-15, 1966 by Edward A. Robin, Manager, Vehicle Test Programming Department.
creator: Robin, Edward A.
source: Saturn V Collection
source: Box 19, Folder 23
source: University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama
date: 1966-10-15
rights: 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: spc_stnv_000225_000249
language: en
type: Text
type: Design Analyses

"Design and Use of Fault Simulation for Saturn Computer Design."
subject: Saturn project
subject: Failure analysis
subject: IBM computer
subject: Logic design
subject: Computerized simulation
description: Describes different aspect of the Fault Simulation for Saturn computer design.
creator: Hardie, F.
creator: Suhocki, R.
source: Saturn V Collection
source: Box 17, Folder 41
source: University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama
date: 1966-06-01
rights: 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: spc_stnv_000225_000249
language: en
type: Text
type: Design Analyses

"Design of the Saturn S-IV Stage Propellant Utilization System."
subject: Saturn project
subject: Liquid propellant rockets
subject: Saturn S-4 stage
description: Describes the SIV vehicle and its components. Presented at: IRE International Convention.
creator: Allen, D. J.
creator: Bekemeyer, L. G.
source: Saturn V Collection
source: Box 6, Folder 55
source: University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama
date: 1962-03-29
rights: 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: spc_stnv_000225_000249
language: en
type: Text
type: Design Analyses

"Design and Development of a 1,500,000-Pound-Thrust Space Booster Engine."
subject: Saturn project
subject: F-1 rocket engine
subject: Liquid propellant rockets
subject: Research and development
subject: Booster rocket engines
description: Describes the F-1 engine design and components.
creator: Aldrich, D. E.
creator: Sanchini, D. J.
source: Saturn V Collection
source: Box 9, Folder 14
source: University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama
date: 1963-07-01
rights: 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: spc_stnv_000225_000249
language: en
type: Text
type: Design Analyses

"Design and Development of a Zero-G Vapor Liquid Separator For Use in Cryogenic Fluid Power Systems."
subject: Saturn project
subject: Cryogenic rocket propellants
subject: Cryogenic fluids
subject: .
description: During long coast periods of zero-gravity, storage vessels for the cryogenic liquids proposed for use in some power transmission systems undergo random distribution of the liquid and vapor phases therein. Thus, when heat flow into the vessel causes the vessel pressure to build-up requiring venting to maintain a safe value, the likelihood of venting the valuable liquid phase, as well as the vapor, results. To preclude this eventuality, various devices for separating the liquid and vapor phases and venting just the vapor have been studied and carried into the experimentation stages.
creator: DiStefano, John F.
creator: Shiozawa, Shiro
source: Saturn V Collection
source: Box 12, Folder 50
source: University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama
date: 1965-01-01
rights: 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: spc_stnv_000225_000249
language: en
type: Text
type: Essays

"Design, Development, and Fabrication of a Prototype Hydraulic Transformer."
subject: Saturn project
subject: Hydraulic equipment pumps
subject: Space vehicles
description: For presentation to the Society of Automotive Engineers, 16 September 1964, Boston, Massachusetts. ABSTRACT: This paper discusses the design, development and fabrication of a prototype hydraulic transformer, Hydro-Aire Model No. 05-055, performed in fulfillment of the requirements of Contract No. NAS 8-5264 for NASA Marshall Space Flight Center. The Hydraulic Transformer described is designed to pump hydraulic oil at a flow of 100 GPM with a pressure rise of 4000 psi, and does this work by utilizing as a power source the flow of RP-1 rocket fuel at a pressure of 1900 psig. The Hydraulic Transformer built to handle this combination of flows and pressures, unprecedented in such devices, has a weight of only 70 pounds for the first development model. The development of this unit is discussed and future development improvements are mentioned.
creator: Morando, Jorge.
creator: Chrysler Corporation. Space Division
source: Saturn V Collection
source: Box 12, Folder 23
source: University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama
date: 1964-09-16
rights: 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: spc_stnv_000225_000249
language: en
type: Text
type: Presentations

"A Description of the ST 124-M Inertial Stabilized Platform and its Application to the Saturn V Launch Vehicle."
subject: Saturn project
subject: Inertial platform
subject: Saturn launch vehicles
subject: Inertial guidance
description: This report is a description of the ST124-M inertial stabilized platform system and its application to the Saturn V launch vehicle. It is a summary report providing the system concept and not a theoretical presentation. Mathematical equations were included only where necessary to describe the equipment; however, the detail derivations supporting these equations were not presented since this was not the theme of the paper.
creator: O'Connor, B. J.
creator: National Aeronautics and Space Administration.
source: Saturn V Collection
source: Box 11, Folder 27
source: University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama
date: 1964-06-26
rights: 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: spc_stnv_000225_000249
language: en
type: Text
type: Reports
identifier: descst124m.pdf NO ADDITIONAL FILE - SAME AS BELOW RECORD