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Preignition phenomena in small A-50/NTO pulsed rocket engines.Preignition phenomena in small Aerozine- 50/nitrogen tetroxide pulsed rocket engines shown partly due to hydrazine nitrate accumulation
Document ID
19670055250
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Christos, T.
James, H. K.
Miron, Y.
Perlee, H. E.
Date Acquired
August 3, 2013
Publication Date
July 1, 1967
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 67-516
Report Number: AIAA PAPER 67-516
Accession Number
67A33979
Distribution Limits
Public
Copyright
Other
Keywords
PROPELLANT COMBUSTION
ROCKET ENGINE
HYPERGOLIC PROPELLANT
HYDRAZINE NITRATE

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