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Hybrid Space Nuclear Reactor Concept
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English
Abstract
A hybrid space nuclear reactor which can provide both electrical power and thermal propulsion has been found to have significant benefits for near term military satellites. It combines the STAR-C thermionic reactor with NERVA rocket propulsion technology. This hybrid reactor would use a W/UO2 cermet core which was developed in the nuclear rocket program of the 1960's. Both the reactor core and the thermionic converters can be tested prior to launch. The design of a 10 kWe reactor capable or producing over 1300 N of thrust is described.
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Citation
Begg, L., Choong, P., Teofilo, V., Dunn, C. et al., "Hybrid Space Nuclear Reactor Concept," SAE Technical Paper 929344, 1992, https://doi.org/10.4271/929344.Also In
References
- Begg L. Otting W Verrill D. “STAR-C Thermionic Space Nuclear Power System” 26 th lntersociety Energy Conversion Engineering Conference Boston, Massachusetts August 1991
- Begg L. Otting W. Wuchte T. “STAR-C Thermionic Space Nuclear Power System” 9 th Symposium on Space Nuclear Power Systems Albuquerque, New Mexico January 1992
- Nuclear Rocket Program Terminal Report Argonne National Laboratory June 30 1966