Cooling of rocket thrust chambers with liquid oxygen

Author:

ARMSTRONG ELIZABETH1,SCHLUMBERGER JULIE1

Affiliation:

1. NASA, Lewis ResearchCenter, Cleveland, OH

Publisher

American Institute of Aeronautics and Astronautics

Reference13 articles.

1. High Pressure Engine Study for Mixed-Mode Vehicle Applications," NASA CR-135141,1977 2 . Rousar. D.C.,and Miller, F. "Cooling with

2. Supercritical Oxygen,"AIAA Paper 75-12$8. Sept. 1975. 3 . Price, H.G."Cooling of High-pressure Rxkct

3. ," . L z - of Spacecraft and Ro-keis. Vol.18,No. 4. July-Aug.1981,pp.338.343. 4 . Price, H.G., and Masters, P.A."Liquid Oxygen

4. Hydrocarbon Fueled Rocket Thrust Chamhers:' AIAA-89-2739. July 1989. 5 . Armstrong, E.S."Liquid Oxygen Cooling of

5. Rocket Engine Liquid Oxygen Technology,"Presented at the XXXVll Congress of the Interna. tional Astronautical Federation, IAF Papt:r 76-174,Oct. 1976.

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