A transpiration-cooled nozzle as applied to a gas core nuclear propulsion system
Aerospace Propulsion Meeting ; 1964 ; Cleveland , OH , U.S.A.
01.01.1964
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Numerical Study of a Transpiration Cooled Rocket Nozzle
British Library Conference Proceedings | 1996
|Numerical study of a transpiration cooled rocket nozzle
AIAA | 1996
|