1–10 von 82 Ergebnissen
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    Electric Aircraft Cryogenic Cooling with Thermo-Acoustic Exergy Management

    R. Dyson | NTIS | 2019
    Schlagwörter: Propulsion system configurations , Propulsion system performance , Temperature control , Fly by wire control

    NASA Acoustic Stirling IRAD Energy Conversion in Aircraft

    R. Dyson | NTIS | 2018
    Schlagwörter: Propulsion system configurations , Temperature control

    Thermo-Fluid Modeling of the Pressurization and Draining of a 1000-Gallon Cryogenic Tank with GFSSP

    A. LaClair / A. Majumdar | NTIS | 2016
    Schlagwörter: Propulsion system performance , Control valves , Temperature

    JSC Advanced Curation: Research and Development for Current Collections and Future Sample Return Mission Demands

    M. D. Fries / C. C. Allen / M. J. Calaway et al. | NTIS | 2015
    Schlagwörter: Environmental control , Solar system , Cryogenic temperature

    Airvolt Aircraft Electric Propulsion Test Stand

    A. Samuel / Y. Lin | NTIS | 2015
    Schlagwörter: Control data (computers) , Control equipment , Propulsion system configurations , Propulsion system performance , Temperature measurement

    Overview of High Temperature Seal Development and Testing Capabilities at the NASA Glenn Research Center

    J. J. Demange / C. S. Taylor / H. P. Dunlap et al. | NTIS | 2014
    Schlagwörter: HIGH TEMPERATURE , HIGH TEMPERATURE ENVIRONMENTS , PROPULSION SYSTEM CONFIGURATIONS , PROPULSION SYSTEM PERFORMANCE , CONTROL SURFACES

    Evaluation of Fast-Time Wake Vortex Models using Wake Encounter Flight Test Data

    N. N. Ahmad / R. L. VanValkenburg / R. L. Bowles et al. | NTIS | 2014
    Schlagwörter: Temperature profiles , Temperature gradients , Air traffic control , National airspace system

    PA Discussion Topics

    H. Dobbs | NTIS | 2011
    Schlagwörter: High temperature , Temperature control , Sil(System integration lab)

    Propulsion System Choices and Their Implications

    C. R. Joyner / D. J. H. Levack / R. E. Rhodes et al. | NTIS | 2010
    Schlagwörter: Propulsion system performance , Temperature control