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  • 1
    facet.materialart.
    Unknown
    In:  Other Sources
    Publication Date: 2011-08-16
    Description: Shaft misalignment effect on accuracy of precision digital shaft angle encoders, using test fixture and optical methods
    Keywords: INSTRUMENTATION AND PHOTOGRAPHY
    Type: ; 20-25, 47 (
    Format: text
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  • 2
    Publication Date: 2019-05-29
    Description: Timing of GEOS satellite xenon beacon flashes
    Keywords: SPACE VEHICLES
    Type: NASA-TM-X-55517 , X-524-66-149
    Format: application/pdf
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  • 3
    Publication Date: 2019-06-27
    Description: Electro-optical observation of magnitude and brightness fluctuations of Pageos satellite during passage
    Keywords: SPACE VEHICLES
    Type: NASA-TM-X-55756 , X-524-66-467
    Format: application/pdf
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  • 4
    Publication Date: 2019-06-27
    Description: Determination of Pageos satellite magnitude and brightness fluctuations
    Keywords: SPACE SCIENCES
    Type: NASA-TM-X-55595 , X-524-66-337
    Format: application/pdf
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  • 5
    Publication Date: 2019-08-13
    Description: The crew functions, instrumentation, and mission profiles for the Spacelab to be flown on board the Shuttle are described. The Spacelab will be operated by up to four scientists or engineers who are not pilots, and who are required to pass only an FAA Class III physical examination to qualify for flight. Of modular design, the Spacelab pallets can house a laboratory for human operation, or experimental pallets for control by either the ground or the Orbiter crew. A shirt sleeve environment is provided by the manned laboratory version, with the crew staying in the Orbiter mid-deck during launch and landing. Electrical power is derived from the Orbiter fuel cells, up to 12 kW for 15 min every three hours and to a total of 890 kWh. Features of the Instrument Pointing System are outlined, along with the data transmission and relay systems and the on-ground check-out facilities.
    Keywords: LAUNCH VEHICLES AND SPACE VEHICLES
    Type: AAS PAPER 82-107 , Goddard Memorial Symposium on Spacelab, Space Platforms and the Future; Mar 17, 1982 - Mar 19, 1982; Greenbelt, MD
    Format: text
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  • 6
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    Unknown
    In:  Other Sources
    Publication Date: 2019-08-28
    Description: A series of experiments directed by NASA for the European Space Agency's Spacelab are planned for early 1983. Spacelab 1 is scheduled to carry equipment for upper atmosphere research and for experiments in plasma and solar physics, medicine, and thermodynamics. Spacelab 2 will provide equipment for research in astronomy, high-energy physics, astrophysics, and solar physics. Spacelab 3 will be equipped to study materials processing in space, biological tests, and cloud physics. Spacelab is modular and reusable, with the planned life equal to 50 missions. The Space Shuttle will carry a Spacelab with scientific equipment of up to 8800 kg into orbits ranging in altitude from 160 to 1100 km and transmitting data at up to 50 Mb/s. The cost of launching a Shuttle/Spacelab mission is estimated at $28 million.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: IEEE Spectrum; 17; May 1980
    Format: text
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  • 7
    Publication Date: 2019-08-28
    Description: It is pointed out that NASA is developing a new way to get payloads into orbit in a short time and at a low cost. The 'Spacelab Hitchhiker' is the carrier program which will accomplish this objective. The Spacelab Hitchhiker carrier is a Shuttle payload. The primary application of the considered program will be related to science and technology payloads. Attention is given to the Hitchhiker concept, details regarding the Hitchhiker-G and Hitchhiker-M, aspects of integration and operations, Orbiter resources and STS interfaces, the conduction of Hitchhiker flights as 'flights of opportunity', questions of payload selection, and organizational interfaces.
    Keywords: SPACE TRANSPORTATION
    Type: AIAA PAPER 85-0504
    Format: text
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