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
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Nuclear Thermal Rocket Propulsion Systems
Online Contents | 2007
|NTIS | 1968
|Nuclear-Thermal-Rocket Propulsion Systems
AIAA | 2008
|Hybrid Rocket Propulsion Performance Prediction
British Library Conference Proceedings | 2005
|Springer Verlag | 1968
|