McDonnell Douglas F-15 Eagle | |
|---|---|
| 国 | 米国 |
| 役割 | 空気優位戦闘機 |
| 初飛行 | 1972年7月27日 |
| 生産 | 1972年~現在 |
| 構築 | 知りません |
ザ マクドネル・ダグラス F-15 イーグル マクドネル・ダグラス(現ボーイング)によって設計されたアメリカの双発、全天候型戦術戦闘機です。提案のレビューに続いて、アメリカ空軍は、専用の航空優位戦闘機のためのサービスの必要性を満たすために1967年にマクドネル・ダグラスの設計を選択しました。イーグルは1972年7月に初飛行し、1976年に就航しました。これは、イスラエル空軍による殺害の大半で、100以上の勝利と空中戦闘での損失なしで、最も成功した現代の戦闘機の一つです
ソース： ウィキペディアのマクドネル ダグラス F-15 イーグル
| 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 |
コーヒーを買って| F-15A Eagle Walk Around | |
|---|---|
| Photographer | Unknow |
| Localisation | Unknow |
| Photos | 17 |
関連項目:
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) |
|---|---|
| 役割 | Air Superiority Fighter |
| National Origin | 米国 |
| メーカー | McDonnell Douglas (now Boeing) |
| Service Entry (F-15C) | 1979 |
| 乗組員 | 1 (Pilot) |
| 長さ | 19.43 m (63 ft 9 in) |
| 翼 | 13.05 m (42 ft 10 in) |
| 高さ | 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.
再生 : 3118
