Last edited by Jusar
Monday, November 16, 2020 | History

3 edition of Results of aeroheating DFI and ET design-data test on a 0.0175-scale model 60-OTS conducted in the Von Karman gas dynamics facility (VKF) 40-inch supersonic and the 50-inch hypersonic wind tunnels A&C (IH-97A/B/C) found in the catalog.

Results of aeroheating DFI and ET design-data test on a 0.0175-scale model 60-OTS conducted in the Von Karman gas dynamics facility (VKF) 40-inch supersonic and the 50-inch hypersonic wind tunnels A&C (IH-97A/B/C)

Results of aeroheating DFI and ET design-data test on a 0.0175-scale model 60-OTS conducted in the Von Karman gas dynamics facility (VKF) 40-inch supersonic and the 50-inch hypersonic wind tunnels A&C (IH-97A/B/C)

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Published by Systems Engineering Division, Johnson Space Center, National Aeronautics and Space Administration in Houston, Tex .
Written in English

    Subjects:
  • Von Karman Institute for Fluid Dynamics.,
  • Hypersonic wind tunnels.,
  • Supersonic wind tunnels.

  • Edition Notes

    StatementJ. Marroquin.
    SeriesNASA-CR -- 167,693., NASA contractor report -- NASA CR-167693.
    ContributionsLyndon B. Johnson Space Center. Systems Engineering Division., Chrysler Corporation. Electronics Products Division. Michoud Engineering Office. Data Management Services.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL16119765M


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Results of aeroheating DFI and ET design-data test on a 0.0175-scale model 60-OTS conducted in the Von Karman gas dynamics facility (VKF) 40-inch supersonic and the 50-inch hypersonic wind tunnels A&C (IH-97A/B/C) Download PDF EPUB FB2