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    Results of investigations on an 0.015-scale 140A/B configuration of the Rockwell International space shuttle orbiter (model 49-O) in the NASA/Ames Research Center 3.5-foot hypersonic wind tunnel (OA36)

    Milam, M. D. / Gillins, R. L. / Cleary, J. W. | NTRS | 1974
    Keywords: Spacecraft Design, Testing And Performance

    Results of an aerodynamic investigation of a space shuttle orbiter/747 carrier vehicle configuration to establish a free-stream data base for ALT separation investigations, utilizing a 0.0125-scale model (48-0/AX1318I-1) in the ARC 14-foot wind tunnel (CA23A)

    Gillins, R. L. | NTRS | 1975
    Keywords: Spacecraft Design, Testing And Performance

    Results of an aerodynamic investigation of a space shuttle orbiter/747 carrier flight test configuration to determine separation characteristics utilizing 0.0125-scale models (48-0/AX1318I-1) in the LTV 4 x 4 foot high speed wind tunnel (CA26), volume 5

    Gillins, R. L. | NTRS | 1976
    Keywords: Spacecraft Design, Testing And Performance

    Results of an aerodynamic investigation of a space shuttle orbiter/747 carrier flight test configuration to determine separation characteristics utilizing 0.0125-scale models (48-0/AX1318I-1) in the LTV 4 x 4 foot high speed wind tunnel (CA26), volume 4

    Gillins, R. L. | NTRS | 1976
    Keywords: Spacecraft Design, Testing And Performance

    Results of an aerodynamic investigation of a space shuttle orbiter/747 carrier flight test configuration to determine separation characteristics utilizing 0.0125-scale models (48-0/AX1318I-1) in the LTV 4 x 4-foot high speed wind tunnel (CA26), volume 3

    Gillins, R. L. | NTRS | 1976
    Keywords: Spacecraft Design, Testing And Performance

    Results of an Aerodynamic Investigation of a Space Shuttle Orbiter/747 Carrier Flight Test Configuration to Determine Separation Characteristics Utilizing 0.0125-Scale Models (48-0/AX1318I-1) in the LTV 4 X 4 Foot High Speed Wind Tunnel (CA26), Volume 2

    Gillins, R. L. | NTRS | 1976
    Keywords: Spacecraft Design, Testing And Performance

    Results of an aerodynamic investigation of a space shuttle orbiter/747 carrier flight test configuration to determine separation characteristics utilizing 0.0125-scale models (48-0/AX1318I-1) in the LTV 4 x 4 foot high speed wind tunnel (CA26), volume 1

    Gillins, R. L. | NTRS | 1976
    Keywords: Spacecraft Design, Testing And Performance

    Airloads investigation of an 0.030-scale model of the space shuttle vehicle 140A/B launch configuration (model 47-OTS) in the ARC 11-foot Unitary Plan Wind Tunnel for Mach range 0.6 to 1.4 (IA14A), volume 11

    Gillins, R. L. | NTRS | 1975
    Keywords: Spacecraft Design, Testing And Performance

    Airloads investigation of an 0.030-scale model of the Space Shuttle Vehicle 140 A/B launch configuration (model 47-OTS) in the ARC 11-foot Unitary Plan Wind Tunnel for MACH range 0.6 to 1.4 (IA14A), volume 10

    Gillins, R. L. | NTRS | 1975
    Keywords: Spacecraft Design, Testing And Performance

    Airloads investigation of an 0.030-scale model of the space shuttle vehicle 140A/B launch configuration (model 47-OTS) in the ARC 11-foot Unitary Plan Wind Tunnel for Mach range 0.6 to 1.4 (IA14A), volume 9

    Gillins, R. L. | NTRS | 1975
    Keywords: Spacecraft Design, Testing And Performance

    Airloads investigation of an 0.030-scale model of the space shuttle vehicle 140A/B launch configuration (model 47-OTS) in the arc 11-foot Unitary Plan Wind Tunnel for Mach range 0.6 to 1.4 (IA14A), volume 8

    Gillins, R. L. | NTRS | 1975
    Keywords: Spacecraft Design, Testing And Performance

    Airloads investigation of an 0.030 scale model of the space shuttle vehicle 140A/B launch configuration (model 47-OTS) in the ARC 11-foot Unitary Plan Wind Tunnel for Mach range 0.6 to 1.4 (IA14A), volume 7

    Gillins, R. L. | NTRS | 1975
    Keywords: Spacecraft Design, Testing And Performance

    Airloads investigation of an 0.030-scale model of the space shuttle vehicle 140A/B launch configuration (model 47-OTS) in the ARC 11-foot Unitary Plan Wind Tunnel for Mach range 0.6 to 1.4 (IA14A), volume 6

    Gillins, R. L. | NTRS | 1975
    Keywords: Spacecraft Design, Testing And Performance

    Airloads investigation of an 0.30-scale model of the space shuttle vehicle 140A/B launch configuration (model 47-OTS) in the ARC 11-foot Unitary Plan Wind Tunnel for Mach range 0.6 to 1.4 (IA14A), volume 5

    Gillins, R. L. | NTRS | 1975
    Keywords: Spacecraft Design, Testing And Performance

    Airloads investigation of an 0.030-scale model of the space shuttle vehicle 140A/B launch configuration (model 47-OTS) in the arc 11-foot unitary plan wind tunnel for Mach range 0.6 to 1.4 (IA14A), Volume 2

    Gillins, R. L. | NTRS | 1975
    Keywords: Spacecraft Design, Testing And Performance

    Airloads investigation of an 0.030-scale model of the space shuttle vehicle 140A/B launch configuration (model 47-OTS) in the arc 11-foot unitary plan wind tunnel for Mach range 0.6 to 1.4 (IA14A), volume 1

    Gillins, R. L. | NTRS | 1975
    Keywords: Spacecraft Design, Testing And Performance

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