Ultrasonic Burn Rate Testing of Bi-Plateau Propellants Under Decreasing Pressure Conditions
41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
01.01.2005
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
SENSITIVITY OF SEVERAL HIGH BURN RATE PROPELLANTS TO ELECTROSTATIC STIMULUS
British Library Conference Proceedings | 1991
|Plateau ballistics in nitrocellulose propellants
AIAA | 1964
|