Oxidizer particle size and binder type effects on nonacoustic combustion instability of solid propellants
Failure of existing theories to correlate experimental nonacoustic combustion instability data
AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, AEROSPACE SCIENCES MEETING, 7TH ; 1969 ; NEW YORK, NY
1970-04-01
Miscellaneous
No indication
English
Nonacoustic instability of composite propellant combustion
Engineering Index Backfile | 1966
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