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The hard start phenomena in hypergolic engines. Volume 1: BibliographyA bibliography of reports pertaining to the hard start phenomenon in attitude control rocket engines on Apollo spacecraft is presented. Some of the subjects discussed are; (1) combustion of hydrazine, (2) one dimensional theory of liquid fuel rocket combustion, (3) preignition phenomena in small pulsed rocket engines, (4) experimental and theoretical investigation of the fluid dynamics of rocket combustion, and (5) nonequilibrium combustion and nozzle flow in propellant performance.
Document ID
19740020114
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
Propulsion Systems
Report/Patent Number
BM-IR-1646-VOL-1
NASA-CR-134313
Report Number: BM-IR-1646-VOL-1
Report Number: NASA-CR-134313
Accession Number
74N28227
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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