巴克斯尔-2

BAC TSR-2

国家英国
作用战术打击/侦察机
首次飞行1964年9月27日
建立2

英国飞机公司 TSR-2 (用于"战术打击和侦察2")是英国飞机公司(BAC)在1950年代末和1960年代初为皇家空军(RAF)研制的一种取消的冷战打击和侦察机。TSR-2旨在以低空和极高速穿透防御良好的前沿战区,然后用核武器或常规武器攻击后方的高价值目标。另一个预期的战斗任务是提供高空、高速对峙、侧视雷达和摄影图像以及信号情报、空中侦察。设计过程中只有一个机身飞行和试飞以及重量上升表明,飞机将无法达到其最初的严格设计规范。由于飞行测试,设计规格降低了。

源: 维基百科上的 BAC TSR-2
TSR.2 Walk Around
PhotographersMichael Benolkin, David Spurgeon-Jackson
LocalisationUnknow
Photos45
等等,为您搜索巴克斯TSR-2.。。
Cosford TSR2 Walk Around
摄影师Unknow
本地化托尼·泰勒
照片37

另请参阅:

第二次世界大战:从闪电战到原子弹的权威视觉历史(DK 权威视觉历史) - 亚马逊 二战地图(DK历史地图) - 亚马逊

BAC TSR-2 Walk Around
摄影师Unknow
本地化未知
照片46

未选择库或已删除库。

BAC TSR.2:鹰的失落明天 - Amazon

BAC TSR-2 Walk Around
摄影师Unknow
本地化未知
照片27

General Characteristics and Role

The BAC TSR-2 (Tactical Strike and Reconnaissance, Mach 2) was an ambitious, highly advanced Cold War aircraft developed for the Royal Air Force (RAF) to replace the English Electric Canberra. Designed under the extensive General Operational Requirement 339 (GOR.339), it was intended to be an all-weather, long-range tactical strike and reconnaissance aircraft capable of operating at both high altitude (Mach 2+) and extremely low altitude (Mach 1.2) using terrain following radar. The project was controversially cancelled in 1965 despite promising flight test results.

Property Typical Value (Prototype/Design)
作用 Tactical Strike and Reconnaissance (TSR) Aircraft
National Origin 英国
制造商 British Aircraft Corporation (Vickers-Armstrong & English Electric)
First Flight 1964年9月27日
船员 2 (Pilot and Navigator/Weapon Systems Operator)
长度 27.13 m (89 ft)
翼展 11.28 m (37 ft)
高度 7.32 m (24 ft)
Maximum Takeoff Weight Approx. 46,357 kg (102,200 lb)

Powerplant and Performance

  • Engines: Two Bristol Siddeley Olympus 22R Mark 320 afterburning turbojet engines.
  • Maximum Thrust (with afterburner): 136.7 kN (30,610 lbf) per engine.
  • Maximum Speed (High Altitude): Mach 2.15 to Mach 2.35 (Planned).
  • Maximum Speed (Low Level): Mach 1.1 to Mach 1.2 (Planned, for terrain following).
  • Ferry Range: Approx. 5,000 km (3,100 mi) with external tanks and in-flight refueling capability.
  • Low-Level Combat Radius: Approx. 1,000 nmi (1,850 km) operating at Mach 0.9.
  • Takeoff Requirement: Designed for short take-off and landing (STOL) capability, aiming for takeoff runs of around 490 meters (1,600 feet) from rough strips using blown flaps.
  • Key Technology: Advanced terrain following radar for high-speed, low-altitude penetration.

Armament and Avionics

  • Internal Armament: One large internal bomb bay.
    • Internal Payload: Up to 2,720 kg (6,000 lb).
    • Weapons: Could carry one large nuclear weapon (like the Red Beard) or multiple smaller tactical nuclear weapons (WE.177) or six 1,000 lb conventional bombs.
  • External Armament: Four underwing pylons.
    • External Payload: Up to 4,500 kg (10,000 lb).
    • Weapons: Could carry additional conventional bombs, WE.177 nuclear weapons, or air-to-surface missiles like the AS.37 Martel.
  • Built-in Armament: None.
  • Avionics: Included an advanced automatic navigation system, Doppler radar, and the terrain following radar essential for its low-level strike role.

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