Boeing X-32 | |
|---|---|
| 국가 | 미국 |
| 역할 | 컨셉 데모 항공기 |
| 첫 비행 | 2000년 9월 18일 |
| 내장 | 2 |
Tthe 보잉 X-32 합동 타격 전투기 경쟁을 위해 설계된 개념 시범 항공기입니다. 록히드 마틴 X-35 시위자에게 패했고, 록히드 마틴 F-35 번개 II로 발전했습니다.
소스: 보잉 X-32 온 위키백과
| Boeing X 32 (Prototype) Walk Around | |
|---|---|
| 사진 작가 | Unknow |
| 로컬라이제이션 | Unknow |
| 사진 | 13 |
Boeing X-32 (Prototype) 1
Boeing X-32 (Prototype) 2
Boeing X-32 (Prototype) 3
Boeing X-32 (Prototype) 4
Boeing X-32 (Prototype) 5
Boeing X-32 (Prototype) 7
Boeing X-32 (Prototype) 6
Boeing X-32 (Prototype) 8
Boeing X-32 (Prototype) 9
잠깐, 당신을 위해 보잉 X-32 검색 ...
참고 항목:
General Characteristics
The Boeing X-32 was a technology demonstrator aircraft developed for the US Joint Strike Fighter (JSF) program, competing against the Lockheed Martin X-35. It was characterized by its single, large delta wing and distinctive, large air intake under the nose.
| Property | Value (X-32A/B Demonstrator) |
|---|---|
| 역할 | JSF Technology Demonstrator (Prototype) |
| 제조업체 | 보잉 |
| First Flight | September 18, 2000 |
| 승무원 | 1 pilot |
| 구성 | Delta wing, single engine, jet |
| Maximum Take-Off Weight | Approx. 17,000 kg (37,500 lb) |
| 윙스 팬 | 10.97 m (36 ft 0 in) |
Propulsion and STOVL System
- Engine: One Pratt & Whitney F119-PW-614S turbofan engine.
- Thrust: Approx. 128 kN (28,000 lbf) (dry) / 192 kN (43,000 lbf) (afterburning).
- STOVL System: Used a direct-lift system. Hot exhaust from the main engine was channeled through two vectoring nozzles located near the aircraft’s center of gravity for vertical lift (Lift Mode).
- Key Feature: The direct-lift system was designed to be simpler, using fewer moving parts than the X-35’s lift fan system, potentially lowering maintenance costs.
Performance and History
- Maximum Speed: Capable of supersonic flight (Mach 1.6+ estimated for production version).
- Supercruise: Demonstrated some level of sustained supersonic capability without afterburner.
- Operational History: The X-32A (conventional) and X-32B (STOVL) prototypes were used to validate Boeing’s technical approach to the JSF requirements (USAF, US Navy, USMC).
- Selection Outcome: In 2001, the Department of Defense selected the Lockheed Martin X-35 (which became the F-35 Lightning II) over the X-32, citing the X-35’s better performance margins and maturity.
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