Design of possible liquid metal cooled reactor for aircraft use, of approximately 9 ft width and 13 ft height; various factors and uncertainties of shielding problem suggest that minimum aircraft size is likely to be of order of 150,000 lb and may well be twice as great; problem of takeoff power; possibility for subsonic aircraft. (See also Aeroplane v 91 n 2358 Nov 9 1956 p 686-7)
Nuclear propulsion for aircraft
Flight
Flight ; 70 , n 2494
1956
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Engineering Index Backfile | 1952
|Nuclear propulsion for aircraft
AIAA | 1967
|Nuclear propulsion for aircraft
Engineering Index Backfile | 1956
|SOME VIEWS ON AIRCRAFT NUCLEAR PROPULSION
SAE Technical Papers | 1959
|