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On the spontaneous ignition of hypergolic propellant systems at low pressures and temperatures.Spontaneous ignition and reaction characteristics of hypergolic propellant pair in low pressure and temperature environment, specifically hydrazine fuel and nitrogen tetroxide atmosphere
Document ID
19650028309
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Choudhury, P. R.
Lee, W.
Merrigan, M. A.
Vango, S. P.
Wilber, P. C.
Date Acquired
August 2, 2013
Publication Date
October 1, 1964
Subject Category
Propellants
Report/Patent Number
CI PAPER 64-29
Report Number: CI PAPER 64-29
Accession Number
65A11013
Funding Number(s)
CONTRACT_GRANT: AF 04/611/-9890
Distribution Limits
Public
Copyright
Other
Keywords
NITROGEN OXIDE
ENVIRONMENTAL CHAMBER
HYDRAZINE
IGNITION LIMIT
HYPERGOLIC PROPELLANT
PROPELLANT COMBUSTION

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