F-15C kotkas

McDonnell Douglas F-15 Eagle

RiikUSA
RolliÕhu paremuse hävitaja
Esimene lend27. juuli 1972
Toodetud1972–tänaseni
EhitatudTeadmata

2007 McDonnell Douglas F-15 kotkas on Ameerika kahemootoriline iga ilmaga taktikaline hävituslennuk, mille on projekteerinud McDonnell Douglas (nüüd Boeing). Pärast ettepanekute läbivaatamist valis Ameerika Ühendriikide õhuvägi 1967. aastal McDonnell Douglase disaini, et rahuldada teenistuse vajadust spetsiaalse õhuüleoleku hävitaja järele. Eagle lendas esmakordselt 1972. aasta juulis ja asus teenistusse 1976. aastal. See on üks edukamaid kaasaegseid hävitajaid, millel on üle 100 võidu ja ilma kaotusteta õhulahingus, kusjuures suurema osa tapmistest on tapnud Iisraeli õhujõud

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General Characteristics and Role

The McDonnell Douglas F-15C Eagle is a legendary American twin-engine, all-weather tactical air superiority fighter. Developed to counter emerging Soviet threats in the late 1960s, the F-15’s design philosophy was succinctly “not a pound for air-to-ground.” The ‘C’ model, introduced in the 1970s, represents an improved single-seat interceptor with greater internal fuel capacity, increased maximum takeoff weight, and enhanced avionics, particularly the AN/APG-63(V) radar system. The F-15 Eagle is renowned for its combat record, holding one of the most successful records in modern aerial warfare with over 100 kills and zero air-to-air losses, proving its mastery of the skies.

Property Typical Value (F-15C)
Rolli Air Superiority Fighter
National Origin Ameerika Ühendriigid
Tootja McDonnell Douglas (now Boeing)
Service Entry (F-15C) 1979
Meeskonna 1 (Pilot)
pikkus 19.43 m (63 ft 9 in)
Tiibade siruulatus 13.05 m (42 ft 10 in)
kõrgus 5.63 m (18 ft 6 in)
Empty Weight 12,700 kg (28,000 lb)
Max Takeoff Weight 30,845 kg (68,000 lb)

Powerplant and Performance

  • Engine: 2 x Pratt & Whitney F100-PW-220 or -220E afterburning turbofans.
  • Thrust (Dry/Afterburner, per engine): 64.9 kN (14,600 lbf) / 105.7 kN (23,770 lbf).
  • Maximum Speed: Mach 2.5+ (2,660 km/h or 1,650 mph) at high altitude.
  • Service Ceiling: 20,000 m (65,000 ft).
  • Range (Ferry): 4,800 km (3,000 mi; 2,600 nmi) with conformal fuel tanks (CFTs) and three external drop tanks.
  • Thrust-to-Weight Ratio: Approximately 1.26:1 (clean configuration), allowing it to accelerate even in a vertical climb.

Armament and Avionics

  • Fixed Armament: 1 x 20 mm M61A1 Vulcan rotary cannon with 940 rounds.
  • Hardpoints (Air-to-Air): 4 underwing, 4 on fuselage stations, 2 on centerline.
  • Missiles: Typically carries a mix of AIM-7 Sparrow (or later AIM-120 AMRAAM) medium-range missiles and AIM-9 Sidewinder short-range missiles.
  • Radar: AN/APG-63 (later upgraded to AN/APG-63(V)1 and V)3 AESA radar), providing excellent long-range detection and tracking capabilities.
  • Conformal Fuel Tanks (CFTs): ‘C’ models can carry two low-drag CFTs, adding significant fuel capacity without completely sacrificing performance.

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