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Hydrogen Peroxide Motor Exhaust Heating to Components at Cryogenic Temperatures in the Vacuum of Space

  • R. L. Pleasant
Conference paper
Part of the Advances in Cryogenic Engineering book series (ACRE, volume 14)

Abstract

The exhaust piume of rocket engines fired In the vacuum of space experiences an extremely wide expansion. The compact packaging on space vehicles, due to weight and space limitations, very often subjects equipment to engine exhaust plume heating. The impingement heating rates cannot be measured In the laboratory because of the difficulty In maintaining a vacuum environment during engine firing and the significant change of plume expansion characteristics due to the presence of a pressure field. On vehicles using cryogenic propeliants, Impingement heating becomes even more important because of the increased temperature potential between exhaust products and cryogenic temperature components and the general requirement to keep heating to the propellants at a minimum.

Keywords

Mach Number Cryogenic Temperature Oblique Shock Main Engine Exhaust Heat 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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Reference

  1. 1.
    L. Feldman, “Vacuum Jet Expansion Program,” General Dynamics/Convair, GDC-BBA66–002 (1966).Google Scholar

Copyright information

© Springer Science+Business Media New York 1969

Authors and Affiliations

  • R. L. Pleasant
    • 1
  1. 1.Convair DivisionGeneral Dynamics CorporationSan DiegoUSA

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