Development of a High Burn Rate Non - Aluminized Composite Propellant with Low Burn Rate Pressure Index
47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
01.01.2011
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Review of Composite Propellant Burn Rate Modeling
AIAA | 1980
|Review of composite propellant burn rate modeling
NTRS | 1979
|Review of composite propellant burn rate modeling
AIAA | 1979
|MEASUREMENT OF FLOW INDUCED BURN RATE AUGMENTATION IN PROPELLANT
British Library Conference Proceedings | 1998
|