Bulk modulus technique for determining void content changes due to solid propellant gas evolution-Reference-Cited by-同舟云学术

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Bulk modulus technique for determining void content changes due to solid propellant gas evolution

Published:1983-06-27 Issue: Volume: Page:
ISSN:
Container-title:19th Joint Propulsion Conference
language:
Short-container-title:

Author:

BECKWITH S.¹,CARROLL H.¹

Affiliation:

1. Hercules, Inc., Hercules Aerospace Div., Magna, UT

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1983-1119

Reference14 articles.

1. D. L. Martin, Effect of Stabilizer Depletion and Critical Pressure Ratio on the Service Life Predictions of Smokeless Propellant - U.S. Amy Missile Command Report TR-RK-76-3, July 1975.

2. D. L. Martin, Service Life Prediction of Smokeless Propellant Motors, U.S. Army Missile Command Report TR-RK-75-6, January 1975.

3. Prediction of the crack lives of solid propellants due to gas accumulation

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. A Novel Approach to Analytically Capture the Change in Propellant Recession Speed due to Propellant Porosity;44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2008-07-21

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