Synonyme wurden verwendet für: growth growth rate
Suche ohne Synonyme: keywords:(specific growth rate control)

1–10 von 10 Ergebnissen
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    Computational and Experimental Efforts in Gravity Probe B Microthruster Analysis

    A. Droege / A. Smith / J. Carter | NTIS | 1996
    Schlagwörter: Satellite attitude control , Mass flow rate , Specific impulse , Thrust control

    A gas handling system for MOMBE growth

    Hersee, S.D. / Ballingall, J.M. | Tema Archiv | 1990
    Schlagwörter: WACHSTUMSRATE , MOMBE GROWTH , THREE-PARAMETER CONTROL

    Performance Characteristics of Vehicles Travelling in Near-Earth Orbits at Supersatellite Velocities

    M. H. Bloom / A. R. Krenkel | NTIS | 1972
    Schlagwörter: Thrust vector control systems , Specific impulse , Burning rate

    Altitude Qualification Test of the Aerojet SVM-6 Solid-Propellant Rocket Motor

    H. L. Merryman / L. R. Smith | NTIS | 1975
    Schlagwörter: Thrust vector control systems , Specific impulse , Burning rate

    Feasibility Demonstration of a Large Impulse Solid Rocket Attitude Control Motor. Volume 1

    N. J. Rolleri | NTIS | 1966
    Schlagwörter: Attitude control systems , Specific impulse , Burning rate

    Thermodynamic and Ballistic Design Fundamentals of Solid-Propellant Rocket Engines

    B. V. Orlov / G. Y. Mazing | NTIS | 1966
    Schlagwörter: Thrust vector control systems , Specific impulse , Burning rate

    MISSILE DEVELOPMENT: TSSAM Production Should Not Be Started as Planned

    T. J. Schultz / R. Dunham / J. F. Seidi | NTIS | 1993
    Schlagwörter: Quality Control & Reliability , Management planning and control , Growth(General) , Low rate

    Test Firing of a Supersonic Probe Thrust Vector Control Concept

    J. R. Ellison | NTIS | 1970
    Schlagwörter: Thrust vector control systems , Specific impulse , Burning rate

    Aging and Surveillance Testing of an Aerojet Minuteman LGM-30G Stage III Rocket Motor at Simulated Pressure Altitude (Motor S/N TMS-10)

    C. H. Kunz / D. E. Franklin | NTIS | 1973
    Schlagwörter: Thrust vector control systems , Specific impulse , Burning rate

    Experimental Investigation of Prepackaged Hybrid Propellant Systems

    J. W. Hamers | NTIS | 1967
    Schlagwörter: Specific impulse , Control systems , Burning rate