Ultrasonic Burn Rate Testing of Bi-Plateau Propellants Under Decreasing Pressure Conditions
41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
2005-01-01
Conference paper
Electronic Resource
English
SENSITIVITY OF SEVERAL HIGH BURN RATE PROPELLANTS TO ELECTROSTATIC STIMULUS
British Library Conference Proceedings | 1991
|Plateau ballistics in nitrocellulose propellants
AIAA | 1964
|