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The hard start phenomena in hypergolic engines. Volume 4: The chemistry of hydrazine fuels and nitrogen tetroxide propellant systemsThe various chemical reactions that occur and that could possibly occur in the RCS engines utilizing hydrazine-type fuel/nitrogen tetroxide propellant systems, prior to ignition (preignition), during combustion, and after combustion (postcombustion), and endeavors to relate the hard-start phenomenon to some of these reactions are discussed. The discussion is based on studies utilizing a variety of experimental techniques and apparatus as well as current theories of chemical reactions and reaction kinetics. The chemical reactions were studied in low pressure gas flow reactors, low temperature homogeneous- and heterogeneous-phase reactors, simulated two-dimensional (2-D) engines, and scaled and full size engines.
Document ID
19750004952
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Miron, Y.
(Bureau of Mines Pittsburgh, PA, United States)
Perlee, H. E.
(Bureau of Mines Pittsburgh, PA, United States)
Date Acquired
September 3, 2013
Publication Date
March 22, 1974
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
BM-IR-1646-VOL-4
NASA-CR-140360
Report Number: BM-IR-1646-VOL-4
Report Number: NASA-CR-140360
Accession Number
75N13024
Funding Number(s)
CONTRACT_GRANT: NASA ORDER T-39882-G
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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