Limitations of two methods of thrust generation, viz, chemical and nuclear heating of working fluid, compared, suggesting that hybrid nuclear chemical propulsion systems may deserve more detailed consideration than hitherto received.
Performance calculations for hybrid nuclear-chemical rocket propulsion systems
ARS -- J
ARS Journal ; 29 , n 3
1959
7 pages
Article (Journal)
English
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Nuclear Thermal Rocket Propulsion Systems
Online Contents | 2007
|NTIS | 1968
|SLUB | 1958
|Nuclear-Thermal-Rocket Propulsion Systems
AIAA | 2008
|Springer Verlag | 1968
|