McDonnell Douglas F-15 Eagle | |
|---|---|
| 국가 | 미국 |
| 역할 | 공기 우위 전투기 |
| 첫 비행 | 1972년 7월 27일 |
| 생산 | 1972년~현재 |
| 내장 | Unknow |
Tthe 맥도넬 더글러스 F-15 이글 맥도넬 더글라스 (현재 보잉)가 설계 한 미국의 트윈 엔진, 전천후 전술 전투기입니다. 제안에 대한 검토에 이어 미국 공군은 1967 년 맥도넬 더글러스 (McDonnell Douglas)의 디자인을 선택하여 전담 공중 우위 전투기에 대한 서비스의 필요성을 충족 시켰습니다. 독수리는 1972년 7월에 처음 비행했고, 1976년에 서비스에 들어갔다. 그것은 가장 성공적인 현대 전투기 중 하나이며, 공중 전투에서 100 회 이상의 승리와 손실이 없으며 이스라엘 공군에 의한 사망의 대부분을 차지합니다.
소스: 맥도넬 더글러스 F-15 이글 위키 백과에
| F-15C Eagle (80-0035) Walk Around | |
|---|---|
| Photographer | Vladimir Yakubov |
| Localisation | Unknow |
| Photos | 41 |
| McDonnell Douglas F-15B Eagle Walk Around | |
|---|---|
| Photographer | Bill Maloney |
| Localisation | Wings of Eagles Discovery Center |
| Photos | 17 |
커피 사줘| F-15A Eagle Walk Around | |
|---|---|
| Photographer | Unknow |
| Localisation | Unknow |
| Photos | 17 |
참고 항목:
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) |
|---|---|
| 역할 | Air Superiority Fighter |
| National Origin | 미국 |
| 제조업체 | McDonnell Douglas (now Boeing) |
| Service Entry (F-15C) | 1979 |
| 승무원 | 1 (Pilot) |
| 길이 | 19.43 m (63 ft 9 in) |
| 윙스 팬 | 13.05 m (42 ft 10 in) |
| 높이 | 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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