La British Aircraft Corporation TSR-2 (para "ataque táctico y reconocimiento 2") fue un avión cancelado de ataque y reconocimiento de la Guerra Fría desarrollado por la British Aircraft Corporation (BAC) para la Royal Air Force (RAF) a finales de la década de 1950 y principios de la década de 1960. El TSR-2 fue diseñado para penetrar en un área de batalla delantera bien defendida a bajas altitudes y velocidades muy altas, y luego atacar objetivos de alto valor en la retaguardia con armas nucleares o convencionales. Otra función de combate prevista era proporcionar alta altitud, alta velocidad de distancia, radar de aspecto lateral e imágenes fotográficas e inteligencia de señales, reconocimiento aéreo. Solo un fuselaje voló y los vuelos de prueba y el aumento de peso durante el diseño indicaron que la aeronave no podría cumplir con sus estrictas especificaciones de diseño originales. Las especificaciones de diseño se redujeron como resultado de las pruebas de vuelo.
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BAC TSR-2 Walk Around
Fotógrafo
Unknow
Localización
Unknow
Fotos
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)
Papel
Tactical Strike and Reconnaissance (TSR) Aircraft
National Origin
Reino Unido
Fabricante
British Aircraft Corporation (Vickers-Armstrong & English Electric)
First Flight
27 de septiembre de 1964
Equipo
2 (Pilot and Navigator/Weapon Systems Operator)
Longitud
27.13 m (89 ft)
Envergadura
11.28 m (37 ft)
Altura
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.