Transpiration cooling of rocket thrust chamber with liquid oxygen-Reference-Cited by-同舟云学术

Transpiration cooling of rocket thrust chamber with liquid oxygen

Published:1998-01-12 Issue: Volume: Page:
ISSN:
Container-title:36th AIAA Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Liu Weiqiang¹,Chen Qizhi¹,Wu Baoyuan²

Affiliation:

1. National Univ. of Defense Technology, Changsha, China

2. 11th Research Inst., Xian, China

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1998-890

Reference4 articles.

1. RudiBeichel'sUniqueDualFuel/DualExpanderReusableRocketEngine. AIAA-96-3127 S. Elizabethet al. CoolingofRocketThrustChamberwith LiquidOxygenAIAA-90-2120

2. Mueggenburg,H.H.etaLPlateletActivelyCooledThermalManagementDevices,AIAA92-3127

3. 159742,N80-14189

4. DieterK.Huzelet al. ModernEngineeringof DesignofLiquid PropellantRocketEngines. 1992,pp86

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