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121–140 von 12,768 Ergebnissen
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    A hydraulic support for free-flight simulation with the Saturn-V Apollo vehicle.

    Von Pragenau, G. L. | NTRS | 1966
    Schlagwörter: VIBRATION TESTING

    HIGH TEMPERATURE PNEUMATIC DUCT SYSTEMS FOR AIRCRAFT

    SAE Technical Papers | 1966
    Schlagwörter: Environmental testing

    Flight testing of advanced spacecraft recovery concepts using the aeromodeler's approach

    Reed, R. D. | NTRS | 1967
    Schlagwörter: Aircraft Design, Testing And Performance

    Techniques for simulating shock and transient loads on unmanned spacecraft

    Forlifer, W. R. | NTRS | 1967
    Schlagwörter: Spacecraft Design, Testing And Performance

    Comparison of lumped parameter models commonly used to describe continuous systems

    Rocke, R. D. | NTRS | 1967
    Schlagwörter: Spacecraft Design, Testing And Performance

    Some transient response and loads problems encountered during design and development of saturn launch vehicles

    Bullock, T. | NTRS | 1967
    Schlagwörter: Spacecraft Design, Testing And Performance

    Transient load problems in unmanned spacecraft

    Kirchman, E. J. | NTRS | 1967
    Schlagwörter: Spacecraft Design, Testing And Performance

    Large parawing development project

    Clemmons, D. L., Jr. | NTRS | 1967
    Schlagwörter: Aircraft Design, Testing And Performance

    Flexible-wing testing techniques and instrumentation

    Hassell, J. L., Jr. | NTRS | 1967
    Schlagwörter: Aircraft Design, Testing And Performance

    Transient response problems of space vehicles

    Rubin, S. | NTRS | 1967
    Schlagwörter: Spacecraft Design, Testing And Performance

    Problems in the measurement of transients

    Kelly, R. D. | NTRS | 1967
    Schlagwörter: Spacecraft Design, Testing And Performance

    Analysis of transient structural response by the method of characteristics

    Chou, P. C. | NTRS | 1967
    Schlagwörter: Spacecraft Design, Testing And Performance

    Some structural considerations in flexible wing design

    Mccomb, H. G., Jr. | NTRS | 1967
    Schlagwörter: Aircraft Design, Testing And Performance

    A new method of numerical integration for some transient response problems

    Howlett, J. T. | NTRS | 1967
    Schlagwörter: Spacecraft Design, Testing And Performance

    Individual flight

    Sobczak, J. W. | NTRS | 1967
    Schlagwörter: Aircraft Design, Testing And Performance

    Reefing tests of a 5-foot (1.524 meter) all-flexible parawing

    Libbey, C. E. | NTRS | 1967
    Schlagwörter: Aircraft Design, Testing And Performance

    A direct approach to the simulation of flight vehicle shock environments

    Ikola, A. L. | NTRS | 1967
    Schlagwörter: Spacecraft Design, Testing And Performance

    Passive and active shock isolation

    Ruzicka, J. E. | NTRS | 1967
    Schlagwörter: Spacecraft Design, Testing And Performance

    NASA space vehicle design criteria program and application to subject area: Transient loads and response

    Jones, G. W., Jr. | NTRS | 1967
    Schlagwörter: Spacecraft Design, Testing And Performance

    Transducers for the measurement of transient motion

    Whittier, R. M. | NTRS | 1967
    Schlagwörter: Spacecraft Design, Testing And Performance