RD-0410
RD-0410 (РД-0410, GRAU index: 11B91) was a Soviet nuclear thermal rocket engine developed from 1965 through the 1980s using liquid hydrogen propellant.[1] The engine was ground-tested at the Semipalatinsk Test Site,[2] and its use was incorporated in the Kurchatov Mars 1994 manned mission proposal.[1]
The hydrogen boost turbopump was designed by KBKhA.[3]
See also
- NERVA, the American project for nuclear thermal propulsion
References
- ^ a b Wade, Mark. "RD-0410". Encyclopedia Astronautica. Retrieved 2009-09-25.
- ^ "«Konstruktorskoe Buro Khimavtomatiky» - Scientific-Research Complex / RD0410. Nuclear Rocket Engine. Advanced launch vehicles". KBKhA - Chemical Automatics Design Bureau. Retrieved 2009-09-25.
- ^ Demyanenko, Y. (July 2005). "Ground Test Demonstrator Engine Boost Turbopumps Design and Development" (PDF). 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Tucson, Arizona: American Institute of Aeronautics and Astronautics, Inc.,. Retrieved 2012-08-21.
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Further reading
- Soviet Mars Propulsion - Nuclear Thermal astronautix.com
- Popular Mechanics article in Russian
- Russian article[dead link]
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