Transient Combustion Response of AP/HTPB Composite Solid Propellant to Acoustic Oscillations in a Rocket Motor
Joint meeting; 37th, Joint Army-Navy-NASA-Air Force; Combustion Subcommittee; JANNAF ; 2000 ; Monterey, CA
2000-01-01
28 pages
Held jointly with the 25th Airbreathing Propulsion Subcommittee and the 19th Propulsion Systems Hazards Subcommittee and 1st Modeling and simulation subcommittee meetings
Aufsatz (Konferenz)
Englisch
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