Developments leading to production of F-89 which is fundamentally an intercepter with additional load of electronic equipment; powered by two Allison J35-A-21 engines; static thrust, rated 4900 lb, afterburning 6800 lb; wing area 562.5 sq ft; span 50 ft; length 50 ft; normal gross weight 32,500 lb; max speed with afterburning 706 mph; service ceiling 52,000 ft; range 2600 mi. (see also Aviation Week v 55 n 8 Aug 20 1951 p 21-2, 25-6)
Northrop F-89 scorpion
Aero Digest
Aero Digest ; 62 , n 1
1951
5 pages
Aufsatz (Zeitschrift)
Englisch
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