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1–20 von 138 Ergebnissen
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    Reentry Body Stability Tests Conducted in Langley Spin Tunnel

    NTRS | 1958
    Schlagwörter: Spacecraft Design, Testing And Performance

    Water Landing Characteristics of a 1/6-Scale Model Reentry Capsule with an 80-Inch Heat Shield

    NTRS | 1959
    Schlagwörter: Spacecraft Design, Testing And Performance

    1/9-Scale Saturn Model

    NTRS | 1960
    Schlagwörter: Spacecraft Design, Testing And Performance

    Landing Energy Dissipation for Manned Reentry Vehicles

    Fisher, Loyd. L. | NTRS | 1960
    Schlagwörter: Spacecraft Design, Testing And Performance

    Landing of Manned Reentry Vehicles

    NTRS | 1961
    Schlagwörter: Spacecraft Design, Testing And Performance

    Effect of Load-Alleviating Structure on the Landing Behavior of a Reentry-Capsule Model

    Hoffman, E. L. / McGhee, J. R. / Stubbs, S. M. | NTRS | 1961
    Schlagwörter: Spacecraft Design, Testing And Performance

    Saturn: A Giant Thrust into Space

    NTRS | 1962
    Schlagwörter: Spacecraft Design, Testing And Performance

    Preliminary Landing Tests of a 1/6-Scale Dynamic Model of a Lunar Excursion Vehicle

    NTRS | 1962
    Schlagwörter: Spacecraft Design, Testing And Performance

    Performance Characteristics of a Preformed Elliptical Parachute at Altitudes between 200,000 and 100,000 Thousand Feet Obtained by In-Flight Photography

    Murro, Harold N. / Whitlock, Charles, H. | NTRS | 1963
    Schlagwörter: Spacecraft Design, Testing And Performance

    Landing Characteristics of a Re-entry Vehicle with a Passive Landing System for Impact Alleviation

    Stubbs, Sandy M. | NTRS | 1963
    Schlagwörter: Spacecraft Design, Testing And Performance

    Dynamic Model Investigation of a 1/20 Scale Gemini Spacecraft in the Langley Spin Tunnel

    Lee, Henry A. / Costigan, Peter J. / Bowman, James S., Jr. | NTRS | 1963
    Schlagwörter: Spacecraft Design, Testing And Performance

    Rendezvous Docking Simulator

    NTRS | 1963
    Schlagwörter: Spacecraft Design, Testing And Performance

    Investigation of the Landing Characteristics of a Re-entry Vehicle Having a Canted Multiple Air Bag Load Alleviation System

    McGehee, John R. / Stubbs, Sandy M. | NTRS | 1963
    Schlagwörter: Spacecraft Design, Testing And Performance

    Aeroelastic Tests of an Eight Percent Scale Saturn C-1 Block II

    NTRS | 1963
    Schlagwörter: Spacecraft Design, Testing And Performance

    Blast Effects of Twin Variable-Cant Rocket Nozzles on Visibility During Landing on a Particle-Covered Surface

    Hurt, G. J. / Lina, L. J. | NTRS | 1964
    Schlagwörter: Spacecraft Design, Testing And Performance

    Dynamic Model Investigation of the Landing Characteristics of a Manned Spacecraft

    Thompson, William C. | NTRS | 1964
    Schlagwörter: Spacecraft Design, Testing And Performance

    Model Investigation of Technique for Full Scale Landing Impact Tests at Simulated Lunar Gravity

    Blanchard, Ulysse J. | NTRS | 1965
    Schlagwörter: Spacecraft Design, Testing And Performance

    Landing Characteristics of the Apollo Spacecraft with Deployed Heat Shield Impact Attenuation Systems

    Stubbs, Sandy M. | NTRS | 1965
    Schlagwörter: Spacecraft Design, Testing And Performance