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  • SPACE TRANSPORTATION  (2)
  • Astronomy  (1)
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  • SPACE TRANSPORTATION  (2)
  • Astronomy  (1)
Years
  • 1
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    The realtime operations of the space shuttle orbiter during rendezvous and proximity operations (1991)
    In:  CASI
    Details
    Publication Date: 2013-08-31
    Description: The Shuttle first demonstrated the capability to perform precision proximity flying in 1983 when the SPAS-01 satellite was deployed and subsequently retrieved. This flight was intended to validate the capability of the Shuttle to perform proximity operations with a co-orbiting vehicle in preparation for the Solar Maximum Repair mission of the next year.
    Keywords: SPACE TRANSPORTATION
    Type: NASA, Washington, NASA Automated Rendezvous and Capture Review. Executive Summary; p 30-31
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 2
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    The real-time operations of the Space Shuttle Orbiter during rendezvous and proximity operations (1991)
    In:  CASI
    Details
    Publication Date: 2013-08-31
    Description: The Space Shuttle Orbiter is the only U.S. spacecraft in operation today that routinely performs an orbital rendezvous with another spacecraft. The trajectory planning and training of both flight crews and ground operations personnel required to achieve a 100 percent success rate is considerable. The preflight planning and training can be reduced through very simple design considerations of a new space vehicle.
    Keywords: SPACE TRANSPORTATION
    Type: NASA, Washington, NASA Automated Rendezvous and Capture Review. A Compilation of the Abstracts; 3 p
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 3
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    Re-Engineering of the Hubble Space Telescope (HST) to Reduce Operational Costs (1996)
    In:  CASI
    Details
    Publication Date: 2019-07-13
    Description: Satellite telemetry processing onboard the Hubble Space Telescope (HST) is carried out using dedicated software and hardware. The current ground system is expensive to operate and maintain. The mandate to reduce satellite ground system operations and maintenance costs by the year 2000 led NASA to upgrade the command and control systems in order to improve the data processing capabilities, reduce operator experience levels and increase system standardization. As a result, a command and control system product development team was formed to redesign and develop the HST ground system. The command and control system ground system development consists of six elements. The results of the prototyping phase carried out for the following of these elements are presented: the front end processor; middleware, and the graphical user interface.
    Keywords: Astronomy
    Type: Paper SO96.6.26 , Proceedings of 4th International Symposium on Space Mission Operations and Ground Data Systems, volume 2; 2; 1088-1095; ESA-SP-394-Vol-2
    Format: text
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    NASA TECHNICAL REPORTS
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