Student Design/Build/Test of a Throttleable LOX-LCH4 Thrust Chamber-Reference-Cited by-同舟云学术

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Student Design/Build/Test of a Throttleable LOX-LCH4 Thrust Chamber

Published:2012-07-30 Issue: Volume: Page:
ISSN:
Container-title:48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Bedard Michael,Feldman Thomas,Rettenmaier Andrew,Anderson William

Publisher

American Institute of Aeronautics and Astronautics

Reference2 articles.

1. 1Dressler, G. "TRW Pintle Engine Heritage and Performance Characteristics," AIAA Paper, 2000.

Cited by 12 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 Numerical Approach to Optimize the Design of a Pintle Injector for LOX/GCH4 Liquid-Propellant Rocket Engine;Aerospace;2023-06-23

2. Characterization of pintle engine performance for GO2/kerosene propellants;Applied Thermal Engineering;2023-06

3. Geometric Effects of Liquid Rocket Engine Pintle Injectors in Supercritical Combustion;International Journal of Aeronautical and Space Sciences;2022-07-19

4. Influence of momentum ratio control mode on spray and combustion characteristics of a LOX/LCH4 pintle injector;Journal of Zhejiang University-SCIENCE A;2022-05

5. Experimental study on the spray characteristics of a gas–liquid pintle injector element;Journal of Visualization;2022-01-14

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