Solid propellant extinguishment by rapid depressurization, investigating motor configuration effect, binder, burning rate catalyst, oxidizer, metal loading and exhaust pressure levels
An experimental investigation of rapid depressurization extinguishment
AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, PROPULSION JOINT SPECIALIST CONFERENCE, 6TH ; 1970 ; SAN DIEGO, CA
1970-06-01
Conference paper
No indication
English