Lockheed XF90 is needle nose, swept wing speed plane with many F-80 Shooting Star features; two Westinghouse J-34-WE-22 axial flow turbojet engines develop 3000 lb static thrust each and feature two turbine stages; gross weight 25,000 lb; extremely thin wing profile used. (see also description by A.MARTHASON, in Aeroplane v 77 n 1986 July 1 1949 p 18-21; and unsigned description in Aero Digest v 59 n 1 July 1949 p 22, 88)
XF-90 newest USAF transonic fighter
Aviation Week
Aviation Week ; 50 , n 21
1949
2 pages
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
XF-90 newest USAF transonic fighter
Engineering Index Backfile | 1949
|XF-90 newest USAF transonic fighter
Engineering Index Backfile | 1949
|Germany's newest fighter bomber
Engineering Index Backfile | 1943
|Parametric Fatigue Analysis of USAF Fighter Aircraft
NTIS | 1970
|A USAF Assessment of STOVL Fighter Options
British Library Conference Proceedings | 1991
|