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101–138 von 138 Ergebnissen
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    Better Way to Fly

    NTRS | 1988
    Schlagwörter: Aircraft Design, Testing And Performance

    AC-67 Press Conference

    NTRS | 1987
    Schlagwörter: Spacecraft Design, Testing And Performance

    Dutch Viking TROS Aktua Special

    NTRS | 1986
    Schlagwörter: Spacecraft Design, Testing And Performance

    Mission Adaptive Wing

    NTRS | 1986
    Schlagwörter: Aircraft Design, Testing And Performance

    Designing Space Station

    NTRS | 1986
    Schlagwörter: Spacecraft Design, Testing And Performance

    Comet Halley Returns. Voyager/Uranus Flyby

    NTRS | 1985
    Schlagwörter: Spacecraft Design, Testing And Performance

    Light Airplane Crash Test at Three Pitch Angles

    Vaughan, Victor L., Jr. / Alfaro-Bou, Emilio | NTRS | 1979
    Schlagwörter: Aircraft Design, Testing And Performance

    First U.S. Mars Landing

    NTRS | 1976
    Schlagwörter: Spacecraft Design, Testing And Performance

    Scaled Lunar Module Jet Erosion Experiments

    Norman S Land / Harland F Scholl | NTRS | 1969
    Schlagwörter: Spacecraft Design, Testing And Performance

    Flight Tests Results from Supersonic Deployment of an 18-Foot Diameter (5.49 meter) Towed Ballute Decelerator

    Mayhue, Robert J. / Eckstrom, Clinton V. | NTRS | 1969
    Schlagwörter: Spacecraft Design, Testing And Performance

    Excerpts from Test Films: Langley Impacting Structures Facility, Lunar Module

    NTRS | 1968
    Schlagwörter: Spacecraft Design, Testing And Performance

    Summary of Attached Inflatable Decelerator (AID) Development

    NTRS | 1968
    Schlagwörter: Spacecraft Design, Testing And Performance

    Flight Test of a 40-Foot Nominal-Diameter Disk-Gap-Band Parachute Deployed at a Mach Number of 1.91 and a Dynamic Pressure of 11.6 Pounds per Square Foot

    Eckstrom, Clinton V. / Preisser, John S. | NTRS | 1968
    Schlagwörter: Spacecraft Design, Testing And Performance

    Performance of a Towed, 48-Inch-Diameter (121.92) Ballute Decelerator Tested in Free-Flight Mach Numbers from 4.2 to 0.4

    Usry, J. W. | NTRS | 1968
    Schlagwörter: Spacecraft Design, Testing And Performance

    Dynamic Model Investigation of Water Pressures and Accelerations Encountered During Landings of the Apollo Spacecraft

    Stubbs, Sandy M. | NTRS | 1967
    Schlagwörter: Spacecraft Design, Testing And Performance

    Gemini 8, This is Houston Flight

    NTRS | 1966
    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

    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

    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

    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

    Rendezvous Docking Simulator

    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

    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

    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

    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

    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

    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

    Reentry Body Stability Tests Conducted in Langley Spin Tunnel

    NTRS | 1958
    Schlagwörter: Spacecraft Design, Testing And Performance