A Unified Model for the Acceleration-Produced Burning Rate Augmentation of Metalized Solid Propellants

Author:

CROWE C. T.

Publisher

Informa UK Limited

Subject

General Physics and Astronomy,Energy Engineering and Power Technology,Fuel Technology,General Chemical Engineering,General Chemistry

Reference9 articles.

1. Crowe , C. T. and Willoughby , P. G. ( 1966 ). Effect of Spin on the Internal Ballistics of a Solid Propellant Rocket Motor. AIAA Paper 66-523 , Los Angeles , Calif .

2. An investigation of the swirling flow in a spinning end-burning rocket

3. Glick , R. L. , Hodge , B. K. and Caveny , L. H. ( 1967 ). Effect of Acceleration on the Burning Rate of Compo-site Propellants , AIAA Paper 67-470 , Washington , D.C .

4. Northam , G. B. ( 1970 ). Effects of the Acceleration Vector on Transient Burning Rate Augmentation of an Aluminized Solid Propellant , AIAA Paper 70-126 , New York , N.Y.

5. Northam , G. B. ( 1971 ). The Effects of Some Propellant Composition Variables on Acceleration Induced Burning-Rate Augmentation of Solid Propellants , presented at the 1971 JANNAF Combined Propulsion Meeting , Las Vegas , Nevada .

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