Hybrid Space Nuclear Reactor Concept

929344

08/03/1992

Event
27th Intersociety Energy Conversion Engineering Conference (1992)
Authors Abstract
Content
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.
Meta TagsDetails
DOI
https://doi.org/10.4271/929344
Pages
6
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.
Additional Details
Publisher
Published
Aug 3, 1992
Product Code
929344
Content Type
Technical Paper
Language
English