Development history of the Apollo reaction control system rocket engine-Reference-Cited by-同舟云学术

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Development history of the Apollo reaction control system rocket engine

Published:1989-07-12 Issue: Volume: Page:
ISSN:
Container-title:25th Joint Propulsion Conference
language:
Short-container-title:

Author:

STECHMAN R.¹,SUMPTER DAVID²

Affiliation:

1. Marquardt Co., Van Nuys, CA

2. Lockheed Missiles and Space Co., Inc., Sunnyvale, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1989-2388

Reference6 articles.

1. Foote, J.F. "Final Report - Apollo SM-LM Engine development Program Summary", Marquardt Report A-1080, Date 10September, 1969 (NASA MSFC Contract NAS90-7281).

2. Anon, "An Investigation of Oxidizer Manifold Explosions", Marquardt Report S-483, 1February 1966.

Cited by 5 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. Hypergolic Propellant Ignition Phenomenon Associated with Two-Phase Oxidizer Flow Injection;Journal of Propulsion and Power;2014-09

2. Test Series to Investigate Oxidizer Manifold Explosions Induced by Condensing Hydrazine–Monomethylhydrazine;Journal of Propulsion and Power;2013-11

3. Liquid Propellant Rocket Engines in the United States (Summary);History of Liquid Propellant Rocket Engines;2006-01

4. History of Liquid Propellant Rocket Engines in the United States;Journal of Propulsion and Power;2003-11

5. Development history of the 25 LBf (110 Newton) Space Shuttle vernierthruster;26th Joint Propulsion Conference;1990-07-16

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