NOP is versatile digital-computer program devoloped for parametric analysis of beryllium-reflected, graphite-moderated nuclear rocket engines. Facilitates analysis of performance of engine with respect to such considerations as specific impulse, engine power, type of engine cycle, and engine-design constraints arising from complications of fuel loading and internal gradients of temperature. Predicts minimum weight for specified performance.
Program For Optimization Of Nuclear Rocket Engines
NASA Tech Briefs ; 18 , 4
1994-04-01
Miscellaneous
No indication
English
Thermal nuclear rocket engines
Online Contents | 2000
Multiple exhaust nozzles for nuclear rocket engines
AIAA | 1966
|Nuclear rocket engines and test facility requirements
AIAA | 1991
|Engineering Index Backfile | 1957
|NTIS | 1968
|