High-pressure calorimeter chamber tests for liquid oxygen/kerosene (LOX/RP-1) rocket combustion
By: Philip A. Masters, Elizabeth S. Armstrong, and Harold G. Price.
Contributors: Armstrong, Elizabeth S.; Price, Harold G.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
Series: NASA technical paper -- 2862.
Publisher: National Aeronautics and Spac14.
Published: 1988
Place of publication: [Washington, DC]
Language: eng
Format: Microform
Subjects: Calorimeters.; Combustion chambers.; High pressure.; Kerosene.; Liquid oxygen.; Oxygen-hydrocarbon rocket engines.; RP-1 rocket propellants.
Other titles: High pressure calorimeter chamber tests for liquid oxygen/kerosene (LOX/RP-1) rocket combustion.
Notes: Distributed to depository libraries in microfiche.

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Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1989] 1 microfiche.