Uncooled nuclear rocket nozzle would provide significant weight, cost, and reliability advantages; current data on materials indicate that composite materials systems would be capable of successful operation in extreme environments imposed on nuclear rocket nozzles; four-basic-composite-materials-systems concept which has been developed under preliminary program sponsored by Martin-Orlando.
Material design concepts for uncooled nuclear rocket nozzles
Matls Science Research
1965
24 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Uncooled Rocket Nozzles for Ultra-High Temperature Propellants
SAE Technical Papers | 1962
|Multiple exhaust nozzles for nuclear rocket engines
AIAA | 1966
|Thermocouple cements for nuclear rocket engine nozzles
Tema Archive | 1969
|AIAA | 1998
|British Library Conference Proceedings | 1998
|