Effect of spin on the internal ballistics of a solid propellant motor
Author:
Affiliation:
1. UNITED AIRCRAFT CORP., UNITED TECHNOLOGY CENTER, SUNNYVALE, CALIF.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1966-523
Reference2 articles.
1. 9 -31.3 1
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1. A Novel Burn Rate Prediction Model of Rotating Solid Rocket Motors;2021 12th International Conference on Mechanical and Aerospace Engineering (ICMAE);2021-07-16
2. Low Burning Rate Aluminized Propellants in Acceleration Fields;AIAA Journal;1984-05
3. Low-burning-rate solid propellants in acceleration fields;17th Joint Propulsion Conference;1981-07-27
4. Transient Period of the Acceleration-Produced Burning Rate Augmentation;AIAA Journal;1976-09
5. Independent Region of Acceleration in Solid Propellant Combustion;AIAA Journal;1974-12
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