Combustion Behavier of a High Burning Rate AP-HTPB Solid Propellant under Transient Pressure Condition-Reference-Cited by-同舟云学术

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Combustion Behavier of a High Burning Rate AP-HTPB Solid Propellant under Transient Pressure Condition

Published:2015-07-23 Issue: Volume: Page:
ISSN:
Container-title:51st AIAA/SAE/ASEE Joint Propulsion Conference
language:
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Author:

Shipeng Li,Wang Ning-fei

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2015-4223

Reference34 articles.

1. 1O'Reilly, P. and Walters, E. "The patriot PAC-3 missile program: An affordable integration approach," Tech. Rep. ADA319957.

2. 2Donnard, R. E. "Antitank Weapon System Application of Impulsive Control and Semiactive Homing," Tech. Rep. AD613185, 1964.

3. 3Cockrell, B. L. "Maneuver Motor Array-Task Completion Report," Tech. Rep. AD917373.

4. 4Li, S., Experiment study and theoretical analysis on the impulsive microthruster, Ph.D. thesis,Beijing Institute of Technology, 2001.

5. 5Caveny, L. H. and Summerfield, M. "Micro-rocket impulsive thrusters," Tech. Rep. AD735381.

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