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  • SPACE VEHICLES  (24)
  • 2015-2019
  • 1970-1974  (24)
  • 1
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    In:  CASI
    Publication Date: 2019-06-27
    Description: The results are reported of research to provide thermal support in the design of the thermal protection system (TPS) of the space shuttles. Tasks discussed include: generation of temperature boundaries for space shuttle orbiter and booster during atmospheric reentry, leading edge and nose cap materials, TPS panel test facility support, thermal test facility support, and hot gas test facility support. A summary of thermal models generated for the space shuttle support is included.
    Keywords: SPACE VEHICLES
    Type: NASA-CR-123813 , LMSC/HREC-D225916 , HREC-5569-3
    Format: application/pdf
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  • 2
    Publication Date: 2019-06-27
    Description: Reusable nuclear shuttle program schedules and logic networks of tasks, sequencing, and interfaces
    Keywords: SPACE VEHICLES
    Type: NASA-CR-103147 , SD-71-466-7
    Format: application/pdf
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  • 3
    Publication Date: 2019-07-13
    Description: Major engineering support provided during the Skylab mission from the Marshall Space Flight Center and its contractors to the Mission Control Center at Houston was essential to Skylab success. The need for this type of support was anticipated during premission preparations due to the complexity and first-flight nature of the Skylab, but the requirements were greatly magnified by the problems encountered early in the mission. The MFSC engineering support organization and its interface to the Mission Control Center is described. The importance of close cooperation between the operating and engineering organizations in this type of mission is discussed. Illustrations are given from more than 1800 systems analysis actions worked out during the nine-month Skylab mission by more than 600 support engineers.
    Keywords: SPACE VEHICLES
    Type: AAS PAPER 74-116 , Annual Meeting; Aug 20, 1974 - Aug 22, 1974; Los Angeles, CA
    Format: text
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  • 4
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    In:  Other Sources
    Publication Date: 2019-07-13
    Description: The reusable Space Tug is a major system planned to augment the Space Shuttle's capability to deliver, retrieve, and support automated payloads. The Space Tug will be designed to perform round-trip missions from low earth orbit to geosynchronous orbit. Space Tug goals and requirements are discussed together with the characteristics of the full capability Tug. The Tug is to be operated in an unmanned 'teleoperator' fashion. Details of potential teleoperator applications are considered, giving attention to related systems studies, candidate Tug mission applications, Tug 'end-effector' alternatives, technical issues associated with Tug payload retrieval, and Tug/payload accommodations.
    Keywords: SPACE VEHICLES
    Type: National Conference on Remotely manned systems: Exploration and operation in space; Sep 13, 1972 - Sep 15, 1972; Pasadena, CA
    Format: text
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  • 5
    Publication Date: 2019-07-13
    Description: Mariner 9 data analysis showed a good performance of the Mars probe planetary approach navigation systems and a good agreement between measured and predicted probe-approach characteristics. It was found that all operations were completed on time and that the calibration of the instruments and the observation of a greater-than-planned number of stars resulted in a higher-than-expected measurement accuracy. The key instruments of the Mariner were TV cameras taking pictures of Phobos and Deimos against a background of stars, calibrated sun and star sensors, and a scan platform. The error models used for optical navigation system elements, the calibration of the scan platform and of the TV cameras, and the image detection and location techniques are discussed in detail.
    Keywords: SPACE VEHICLES
    Type: AIAA PAPER 72-866 , American Institute of Aeronautics and Astronautics, Guidance and Control Conference; Aug 14, 1972 - Aug 16, 1972; Stanford, CA
    Format: text
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  • 6
    Publication Date: 2019-06-27
    Description: The critical thermal control problems and verification of thermal mathematical model results for the space shuttle concept are discussed. The use of a small scale thermal model of the space shuttle is proposed. It was determined that a one-third scale model of the space shuttle would serve as a useful tool throughout the entire thermal design and verification program. The major considerations in modeling the conduction-radiation-convection fields, the level of detail for modeling various systems, preliminary test requirements, and potential applications of the thermal scale model are summarized.
    Keywords: SPACE VEHICLES
    Type: NASA-CR-128849 , LMSC-D313907 , TP-3613
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  • 7
    Publication Date: 2019-07-13
    Description: Orbital space station program, discussing common module design, support, space shuttles and objectives
    Keywords: SPACE VEHICLES
    Type: SAE PAPER 700755 , SOCIETY OF AUTOMOTIVE ENGINEERS, NATIONAL AERONAUTIC AND SPACE ENGINEERING AND MFG. MEETING; Oct 05, 1970 - Oct 09, 1970; LOS ANGELES, CA
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  • 8
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    In:  Other Sources
    Publication Date: 2019-07-13
    Description: The reusable space tug is a major system being planned for use with the space shuttle to augment its capability to deliver, retrieve, and support automated payloads. The reusable space tug will be designed to support all the planned missions beyond low earth orbit including geosynchronous orbit. Tug missions and requirements are discussed together with tug options, giving attention to existing transfer stages and growth stages. System studies for an interim tug concept are planned to begin in February 1973. Three independent studies will be conducted: two on cryogenic tugs and one on storable propellant tugs.-
    Keywords: SPACE VEHICLES
    Type: AIAA PAPER 73-74 , Annual Meeting and Technical Display; Jan 08, 1973 - Jan 10, 1973; Washington, DC
    Format: text
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  • 9
    Publication Date: 2019-06-27
    Description: Electrical power distribution systems for space vehicle with isotope/Brayton source
    Keywords: SPACE VEHICLES
    Type: NASA-CR-103072
    Format: application/pdf
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  • 10
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    In:  Other Sources
    Publication Date: 2011-08-16
    Description: The scientific objectives of the Explorer-45 mission are discussed. The primary objective is the study of the ring current responsible for the main phase of magnetic storms. Closely associated with this objective is the determination of the relationship between magnetic storms, substorms, and the acceleration of charged particles in the magnetosphere. Further objectives are the measurement of a wide range of proton, electron and alpha-particle energies, and studies of wave-particle interactions responsible for particle transport and loss in the inner magnetosphere. The orbital parameters, the spacecraft itself, and some of its unique features, such as the data handling system, which is programmable from the ground, are described.
    Keywords: SPACE VEHICLES
    Type: Journal of Geophysical Research; 78; Aug. 1
    Format: text
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