1–16 von 16 Ergebnissen
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    A Chemically Fueled Propulsion System for Deep Submergence

    Howell, H. L. | SAE Technical Papers | 1961

    Qualification of the Space Shuttle Orbiter Radiator System

    Howell, H. R. / Williams, J. L. | SAE Technical Papers | 1982

    Transient Thermal Performance Prediction of the Lunar Module Environmental Control System

    Howell, H. R. / Williams, J. L. | SAE Technical Papers | 1969

    Hand-printed input for on-line systems

    Bernstein, M. I. / Howell, H. L. | TIBKAT | 1969

    Inverter-converter parallel operation

    Ernsberger, G. W. / Howell, H. R. / Klingenberger, J. L. | TIBKAT | 1969

    Pressurized-Flat-Interface Heat Exchanger

    Voss, F. E. / Howell, H. R. / Winkler, R. V. | NTRS | 1990

    Inverter-converter parallel operation

    Ernsberger, G. W. / Howell, H. R. / Klingenberger, J. L. | NTRS | 1969

    Revised Lunar Module Ascent Stage Thermal Model handbook

    De Laughter, D. A. / French, R. J. / Howell, H. R. | NTRS | 1970

    Parallel operation of aerospace static inverters.

    Ernsberger, G. W. / Gourash, F. / Howell, H. R. et al. | NTRS | 1965

    Challenges in the development of the orbiter radiator system

    Williams, J. L. / Oren, J. A. / Modest, M. F. et al. | NTRS | 1985

    Utilization of 3-D CADD in Analysis, Design, and Construction of Mobile Service Tower for Atlas Launch Vehicles

    Bobczynski, N. / Wrona, M. / Hansen, D. et al. | British Library Conference Proceedings | 1996

    A Low-Cost, High-Performance VTOL for the General Aviation Marketplace

    Barrie, R. / Howell, H. / Labows, S. et al. | British Library Conference Proceedings | 2000