
Boeing X-32 | |
|---|---|
| 国家 | 美国 |
| 作用 | 概念演示飞机 |
| 首次飞行 | 2000年9月18日 |
| 建立 | 2 |
这 波音X-32 是专为联合打击战斗机比赛设计的概念演示飞机。它输给了洛克希德马丁X-35演示者,这进一步发展成洛克希德马丁F-35闪电II。
源: 维基百科上的波音X-32
| Boeing X 32 (Prototype) Walk Around | |
|---|---|
| 摄影师 | Unknow |
| 本地化 | 未知 |
| 照片 | 13 |
等等, 为你搜索波音 X - 32...

另请参阅:
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) |
|---|---|
| 作用 | JSF Technology Demonstrator (Prototype) |
| 制造商 | 波音 |
| First Flight | September 18, 2000 |
| 船员 | 1 pilot |
| 配置 | Delta wing, single engine, jet |
| Maximum Take-Off Weight | Approx. 17,000 kg (37,500 lb) |
| 翼展 | 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.
视图 : 1430


















