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    Evaluation of Transient Pin-Stress Requirements for Spacecraft Launching in Lightning Environments. Pain Free Analysis to Alleviate Those Pin Stress Headaches

    Edwards, Paul / Terseck, Alex / Trout, Dawn | NTRS | 2016
    circuits is dependent on the umbilical current drive, the cable transfer impedance and the source/ load circuitry, and the reference potential used ...
    Schlagwörter: Electronics And Electrical Engineering

    NASA's Space Launch System Advanced Booster Engineering Demonstration and Risk Reduction Efforts

    Crumbly, Christopher M. / May, Todd / Dumbacher, Daniel | NTRS | 2012
    -sized for mission requirements. NASA developed the Advanced Booster Engineering Demonstration and/or Risk Reduction NRA to seek industry ...

    NASA's Space Launch System Advanced Booster Engineering Demonstration and/or Risk Reduction Efforts

    Crumbly, Christopher M. / Dumbacher, Daniel L. / May, Todd A. | NTRS | 2012
    right-sized for mission requirements. NASA developed the Advanced Booster Engineering Demonstration and/or Risk Reduction NRA to seek industry ...

    Copper-Water and Hybrid Aluminum-Ammonia Heat Pipes for Spacecraft Thermal Control Applications

    Ababneh, Mohammed T. / Tarau, Calin / Anderson, William G. et al. | NTRS | 2018
    handle heat flux requirements for spacecraft thermal control applications. The 5-10 W/cm2 heat density limitation of aluminum-ammonia grooved ...
    Schlagwörter: Engineering (General)

      Copper-Water and Hybrid Aluminum-Ammonia Heat Pipes for Spacecraft Thermal Control Applications

      Ababneh, Mohammed T. / Tarau, Calin / Anderson, William G. et al. | NTRS | 2018
      handle heat flux requirements for spacecraft thermal control applications. The 5-10 W/cm2 heat density limitation of aluminum-ammonia grooved ...
      Schlagwörter: Engineering (General)

    Attitude Ground System (AGS) For The Magnetospheric Multi-Scale (MMS) Mission

    Raymond, Juan C. / Sedlak, Joseph E. / Vint, Babak | NTRS | 2015
    -dimensional study of the phenomenon of magnetic reconnection, which is the primary objective of the mission. The MMS spacecraft were launched early on ...

    The Importance of Technology Readiness in NASA Earth Venture Missions

    Wells, James E. / Komar, George J. | NTRS | 2009
    mature technology that has been modeled or demonstrated in a relevant environment (Technology Readiness Level (TRL) >5). Technology Readiness ...

    Z-Pinch Magneto-Inertial Fusion Propulsion Engine Design Concept

    Miernik, Janie H. / Statham, Geoffrey / Adams, Robert B. et al. | NTRS | 2011
    industry, as well as in fusion energy research. There is a wealth of literature characterizing Z-Pinch physics and existing models (3-5). In order ...