Reusable launch vehicle propulsion based on the RD-0120 engine-Reference-Cited by-同舟云学术

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Reusable launch vehicle propulsion based on the RD-0120 engine

Published:1995-07-10 Issue: Volume: Page:
ISSN:
Container-title:31st Joint Propulsion Conference and Exhibit
language:
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Author:

Goncharov N,Orlov V,Rachuk V,Shostak A,Starke R

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1995-3003

Reference5 articles.

1. Y.A., and Sciorelli,F.A. "Design, Development, and Historyof theOxygen/HydrogenEngineRD0120,"AIAA PaperNo. 95-2540,July 1995.

2. Gontcharov, N.S., Hulka, I., and Dexter, C. "Development Status of a Soot-Free Fuel-Rich Kerosene Tripropellant Preburner for Reusable LiquidRocketEngineApplications,"AIAAPaper No.95-3002,July 1995.

3. FY95 FY96 -97 FY98

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