Last edited by Faegore
Friday, July 31, 2020 | History

3 edition of Results of the Space Shuttle Vehicle Ascent Air Data System probe calibration test using a 0.07-scale external tank forebody model (68T) in the AEDC 16-foot transonic wind tunnel (I.A.-310). found in the catalog.

Results of the Space Shuttle Vehicle Ascent Air Data System probe calibration test using a 0.07-scale external tank forebody model (68T) in the AEDC 16-foot transonic wind tunnel (I.A.-310).

Results of the Space Shuttle Vehicle Ascent Air Data System probe calibration test using a 0.07-scale external tank forebody model (68T) in the AEDC 16-foot transonic wind tunnel (I.A.-310).

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Published by National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, National Technical Information Service, distributor in Houston, Tex, [Springfield, Va.? .
Written in English

    Subjects:
  • Space shuttles.

  • Edition Notes

    Statementby J.G.R. Collette.
    SeriesNASA-CR -- 167,696., NASA contractor report -- NASA CR-167696.
    ContributionsLyndon B. Johnson Space Center.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL15364432M


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Results of the Space Shuttle Vehicle Ascent Air Data System probe calibration test using a 0.07-scale external tank forebody model (68T) in the AEDC 16-foot transonic wind tunnel (I.A.-310) Download PDF EPUB FB2