Combustion instability -- departures from normal steady-state operating pressure -- has been major problem in solid propellant rocket motor design since early in World War II; experimental work and present state of art are briefly summarized; various theories discussed, with special attention to McClure theory.
Combustion instability in solid propellant rocket motors -- Review
Fuel Soc J
Fuel Society Journal ; 14
1963
12 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Combustion instability in solid propellant rocket motors
Engineering Index Backfile | 1958
|