Burning rate of AP/HTPB base-bleed composite propellant under free ambient pressure
Aerospace science and technology ; 62 ; 31-35
2017
Aufsatz (Zeitschrift)
Englisch
Molybdenum Trioxide effects on HTPB/AP/A1 Based Propellant Burning Rate
British Library Conference Proceedings | 2002
|AIAA | 1981
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