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    Wind Tunnel Tests of the 0.010-Scale Space Shuttle Integrated Vehicle (Model 52-QT) in the NASA/Ames 3.5-Foot Hypersonic Wind Tunnel (IA18)

    V. Esparza / E. Chee / J. Stone et al. | NTIS | 1975
    Schlagwörter: Aerodynamic characteristics , Spacecraft configurations