Boeing X-32 | |
|---|---|
| 国 | 米国 |
| 役割 | コンセプトデモンストレーター機 |
| 初飛行 | 2000年9月18日 |
| 構築 | 2 |
ザ ボーイングX-32 は、ジョイントストライクファイター競技のために設計されたコンセプトデモンストレーター機です。ロッキード・マーティンX-35デモンストレーターに敗れ、ロッキード・マーティンF-35ライトニングIIにさらに発展しました。
ソース： ウィキペディアのボーイング X-32
| Boeing X 32 (Prototype) Walk Around | |
|---|---|
| カメラマン | Unknow |
| ローカライズ | 知りません |
| 写真 | 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
待って、検索ボーイングX-32.
関連項目:
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) |
|---|---|
| 役割 | JSF Technology Demonstrator (Prototype) |
| メーカー | ボーイング |
| First Flight | September 18, 2000 |
| 乗組員 | 1 pilot |
| Configuration | Delta wing, single engine, jet |
| Maximum Take-Off Weight | Approx. 17,000 kg (37,500 lb) |
| 翼 | 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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