Critical examinations of North American F-LOOA Super Sabre; wing has leading edge sweep of 45°; structure permits relatively easy and rapid manufacture; engine is Pratt and Whitney J57-P-7, split compressor turbojet, weighing 4500 lb and giving 10,000 lb thrust; armament comprises four 20-mm M-39 rapid firing cannon in lower part of nose.
Supersonic fighter
Flight
Flight ; 67 , n 2417
1955
5 pages
Aufsatz (Zeitschrift)
Englisch
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