An Overview of Nuclear Thermal Propulsion Graphite, Composite, and CERMET Designs for Thrust Sizes 10,000 to 250,000-pounds
45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit ; 2009 ; Denver , Colorado
2009-01-01
Conference paper
Electronic Resource
English
Increasing cermet fuel thermal margin with Thoria for nuclear thermal propulsion
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