Synonyms were used for: Wind Wind tunnel tunnel
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    Space Shuttle Abort Separation Pressure Investigation. Volume 1, Part B Booster Data at Mach 5

    L. L. Trimmer / D. A. Love / J. M. Rampy et al. | NTIS | 1972
    Keywords: Wind tunnel stability tests , Wind tunnel models

    Computer-Aided Space Shuttle Orbiter Wing Design Study

    W. P. Phillips / J. P. Decker / T. R. Rau et al. | NTIS | 1974
    Keywords: Hypersonic wind tunnels , Wind tunnel tests

    Space Shuttle Space Shuttle Abort Separation Pressure Investigation. Volume 2, Part a Orbiter Data at Mach 5

    L. L. Trimmer / D. A. Love / J. M. Rampy et al. | NTIS | 1972
    Keywords: Wind tunnel models

    Influence of Configuration Details on the Subsonic Characteristics of a Space Shuttle Orbiter Design

    J. P. Decker / W. P. Phillips | NTIS | 1974
    Keywords: Wind tunnel tests

    Space Shuttle Abort Separation Pressure Investigation. Volume 1, Part a Booster Data at Mach 5

    L. L. Trimmer / D. A. Love / J. M. Rampy et al. | NTIS | 1972
    Keywords: Wind tunnel models

    Space Shuttle Abort Separation Pressure Investigation. Volume 2, Part B Orbiter Data at Mach 5

    L. L. Trimmer / D. A. Love / J. M. Rampy et al. | NTIS | 1972
    Keywords: Wind tunnel stability tests

    Space Shuttle Abort Separation Pressure Investigation. Volume 6 Orbiter Data at Mach 2

    L. L. Trimmer / D. A. Love / J. M. Rampy et al. | NTIS | 1972
    Keywords: Wind tunnel stability tests

    Space Shuttle Abort Separation Pressure Investigation. Volume 5 Booster Data at Mach 2

    L. L. Trimmer / D. A. Love / J. M. Rampy et al. | NTIS | 1972
    Keywords: Wind tunnel stability tests

    Space Shuttle Abort Separation Pressure Investigation. Volume 3 Booster Data at Mach 3

    L. L. Trimmer / D. A. Love / J. M. Rampy et al. | NTIS | 1972
    Keywords: Wind tunnel stability tests

    Space Shuttle Abort Separation Pressure Investigation. Volume 4 Orbiter Data at Mach 3

    L. L. Trimmer / D. A. Love / J. M. Rampy et al. | NTIS | 1972
    Keywords: Wind tunnel stability tests