North American F-107A :Fighter-bomber 1957 U.S.A.F

How to controll


H:heading C:reset
P:pitching 1:stereo on
R:rolling 2:stereo off

SPECIFICATIONS: IIIE
Wingspan: 11.20m
length: 18.50m
height: 6.00m
empty mass: 16,852kg
start mass: 22,204kg
engine: Prrat&Whitney J-75-P9(9,300kg)
max speed: 2,200km/h
initial climb: 4,880m/min
ceiling: 15,250m
range w/max.fuel: 1,900km
armament: 20mmMGX4, bombs: 4,540kg
Crew: 1
背部に空気取り入れ口を持つ非常にユニークなデザインです。原型はF100でその発展型として設計されアメリカ空軍のF100の後継機としてF105と正式採用の座を争いました。空力的にも、また速度もF105より優れていましたが兵器搭載量とその搭載バリエーションが劣った結果、その競争には敗れました。正式採用されない場合、通常は正式採用コードを与えられませんが空軍はその優秀さに注目してテストを継続するためF-107Aという正式コードを与えています。
 
 
The YF-107A was originally designed as a tactical fighter-bomber version of the F-100, and was entered into a competition sponsored by the Air Force. Originally designated the F-100B, the aircraft featured a recessed weapons bay under the fuselage, as well as an all-moving vertical fin and a control system which permitted the plane to roll at supersonic speeds. The aircraft's most distinguishing feature is its Variable Area Inlet Duct, mounted in an unconventional position directly above and just behind the cockpit, which automatically controlled the amount of air fed to the jet engine. The air intake was located overhead and behind to prevent it from interfering with the aircraft's weapon's control and guidance radar. Extensive design changes resulted in its redesignation from F-100B to YF-107A before the first prototype flew.
 
 

Copyright c 2006 b-side-museum.com