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Saturday, August 1, 2020 | History

3 edition of Independent Orbiter assessment found in the catalog.

Independent Orbiter assessment

Independent Orbiter assessment

analysis of the backup flight system

  • 115 Want to read
  • 12 Currently reading

Published by McDonnell Douglas Astronautics Company, Houston Division, National Aeronautics and Space Administration in Houston, Tex, [Washington, DC .
Written in English

    Subjects:
  • Space shuttles.,
  • Airborne/spaceborne computers.,
  • Applications programs (Computers),
  • Circuit breakers.,
  • Circuits.,
  • Display devices.,
  • Failure modes.,
  • Flight control.,
  • Protectors.,
  • Space shuttle orbiters.,
  • Spacecraft control.,
  • Spacecraft reliability.,
  • Switches.

  • Edition Notes

    Other titlesAnalysis of the backup flight system.
    Statement[prepared by E.E. Prust, L.W. Hinsdale, R.W. Mielke].
    SeriesNASA-CR -- 185567., NASA contractor report -- NASA CR-185567.
    ContributionsHinsdale, L. W., Mielke, R. W., McDonnell Douglas Astronautics Company--Houston Division., United States. National Aeronautics and Space Administration.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL18263415M

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Independent Orbiter assessment Download PDF EPUB FB2

Independent Orbiter Assessment Assessment of the Manned Maneuvering Unit FMEA/CIL I. 0 EXECUTXVE SUMMARY The McDonnell Douglas Astronautics Company (MDAC) was selected in June to perform an Independent Orbiter Assessment (IOA) of the Failure Modes and Effects Analysis (FMEA) and Critical Items List (CIL).

independent Orbiter Assessment Analysis of the Body Flap Subsystem EXECUTIVE SUMMARY The McDonnell Douglas Astronautics Company (MDAC) was selected in June to perform an Independent Orbiter Assessment (IOA) of the Failure Modes and Effects Analysis (FMEA) and Critical Items List (CIL).

Direction was given by the STS Orbiter and GFE. The item Independent Orbiter assessment: analysis of the rudder/speed brake subsystem, [prepared by R.E. Wilson, J.R. Riccio] represents a specific, individual, material embodiment of a distinct intellectual or artistic creation found in Indiana State Library.

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The results of the Independent Orbiter Assessment (IOA) of the Failure Modes and Effects Analysis (FMEA) and Critical Items List (CIL) is presented.

The IOA effort first. Get this from a library. Independent Orbiter assessment: analysis of the purge, vent and drain subsystem. [M C Bynum; McDonnell Douglas Astronautics Company--Houston Division.; United States.

National Aeronautics and Space Administration.]. The results of the Independent Orbiter Assessment (IOA) of the Failure Modes and Effects Analysis (FMEA) and Critical Items List (CIL) are presented.

The IOA effort first completed an analysis of the Nose Wheel Steering (NWS) hardware, generating draft failure modes and potential critical items.

The statement of task for the National Research Council’s (NRC’s) Committee to Review Near-Earth Object Surveys and Hazard Mitigation Strategies required it to “include an assessment of the costs of various alternatives, using independent cost estimating.” Science Applications International.

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Jun 12,  · With the orbiter returning covered in skin and the inside stuffed with living tissue, and evidence of the Venture having landed on Mars, and only one of its crew returning - near catatonic - the team constructs a myriad of scenarios to explain the unexplainable.

But, alas, the ending is pat and full of hope, but without any real payoff/5(34). Full text of "Independent Orbiter Assessment (IOA): Assessment of the communication and tracking subsystem, volume 1" See other formats.

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