Last edited by JoJozshura
Monday, May 4, 2020 | History

3 edition of A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis found in the catalog.

A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis

A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis

  • 149 Want to read
  • 40 Currently reading

Published by National Aeronautics and Space Administration, National Technical Information Service, distributor in [Washington, D.C.], [Springfield, Va .
Written in English

    Subjects:
  • Combustion chambers.,
  • Cooling systems.,
  • Engine coolants.,
  • Heat exchangers.,
  • Heat transfer.,
  • Hydrogen oxygen engines.,
  • Rocket engines.

  • Edition Notes

    StatementKenneth J. Kacynski, John M. Kazaroff, and Robert S. Jankovsky.
    SeriesNASA technical memorandum -- 104430.
    ContributionsKazaroff, John M., Jankovsky, Robert S., United States. National Aeronautics and Space Administration.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL15399333M


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A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis Download PDF EPUB FB2

Get this from a library. A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis. [Kenneth J Kacynski; John M Kazaroff; Robert S Jankovsky; United States. National Aeronautics and. A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis (SuDoc NAS ) [Kenneth J.

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A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis / Kenneth J. Kacynski, John M. Kazaroff, and Robert S. Jankovsky. Author. Kacynski, Kenneth J. Other Authors. Kazaroff, John M. Jankovsky, Robert S. United States. National Aeronautics and Space Administration. Published. A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis [microform] / Kenneth J.

Kacynski, John M. Kazaroff, and Robert S. Jankovsky National Aeronautics and Space Administration ; National Technical Information Service, distributor [Washington, D.C.]: [Springfield, Va. Buy A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis (SuDoc NAS ) by Kenneth J.

Kacynski (ISBN:) from Amazon's Book Store. Author: Kenneth J. Kacynski. Publishing History This is a chart to show the publishing history of editions of works about this subject. Along the X axis is time, and on the y axis is the count of editions published.

A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis by: Kacynski, Kenneth J. Published: () Cooling of rocket thrust chambers with liquid oxygen by: Armstrong, Elizabeth S. A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis Kenneth John Kacynski Not In Library.

Journal of Propulsion and Power; Journal of Spacecraft and Rockets; A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis. KENNETH KACYNSKI, Aerodynamic and heat transfer analysis of the low aspect ratio turbine using a 3D Navier-Stokes code.

CHOI and. Experimental evaluation of heat transfer on a 1 area ratio rocket nozzle [microform] / Kenneth J. Kacynski, Albert J. Pavli, and Tamara A. Smith National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service] [Washington, D.C.]: [Springfield, Va hydrogen rocket engines Download hydrogen rocket engines or read online here in PDF or EPUB.

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A Dual Cooled Hydrogen Oxygen Rocket Engine Heat Transfer Analysis Analysis Of The Transient Radiation Heat Transfer Of An Uncooled Rocket Engine Operating Outside Earth S Atmosphere. Share & Embed. Embed Script.

Size (px). 1 Technical Paper The prediction of nozzle performance and heat transfer in hydrogen/oxygen rocket engines with transpiration cooling, film cooling, and high area ratios Kacynski, Kenneth J.

Full text of "NASA Technical Reports Server (NTRS) Bibliography of Lewis Research Center Technical Publications announced in " See other formats. The group produced many papers that described injector designs based on different geometries A paper by John Wanhainen, Harold Parish, and William Conrad, Effect of Propellant Injection Velocity on Screech in 20, Pound Hydrogen-Oxygen Rocket Engine, contained the first full description of the RETFs design and operation This report.

7 Technical Paper A Dual-Cooled Hydrogen-Oxygen Rocket Engine Heat Transfer Analysis Kacynski, Kenneth J., Kazaroff, John M., Jankovsky, Robert S.

Dual nozzle single pump fuel injection system. SciTech Connect. Gonzalez, C. This patent describes an improvement in a fuel injection system in a stratified charge hyb. 10 Technical Paper A Dual-Cooled Hydrogen-Oxygen Rocket Engine Heat Transfer Analysis Kacynski, Kenneth J., Kazaroff, John M., Jankovsky, Robert S.

National Aeronautics and Space Adminstration.