BAC TSR-2

BAC TSR-2
Zemlja	Velike britanije
Ulogu	Taktički udar/izviđački avioni
Prvi let	27 Septembar 1964
Izgradio	2

Britanska korporacija za avione TSR-2 (za "taktički udar i izviđanje 2") bio je otkazani hladnoratovski štrajk i izviđački avion koji je razvila Britanska korporacija za avione (BAC) za Kraljevsko vazduhoplovstvo (RAF) krajem pedesetih i početkom šezdesetih godina prošlog veka. TSR-2 je dizajniran da probije dobro odbranjenu prednju borbenu oblast na malim visinama i veoma velikim brzinama, a zatim napada visoko vredne ciljeve u pozadini nuklearnim ili konvencionalnim oružjem. Druga nameravana borbena uloga bila je da se obezbede visoke visine, brzo stajanje, radari bočnog izgleda i fotografske slike i signali inteligencije, izviđanja iz vazduha. Samo jedan avion je leteo i testirao letove i dizanje težine tokom projektovanja nagovestilo je da letelica neće moći da ispuni svoje prvobitne stroge specifikacije dizajna. Specifikacije dizajna su smanjene kao rezultat testiranja leta.

Izvor: BAC TSR-2 na Vikipediji

TSR.2 Walk Around
Photographers	Michael Benolkin, David Spurgeon-Jackson
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Photos	45

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Cosford TSR2 Walk Around
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Lokalizacija	Toni Tejlor
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TSR2 Cosford

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BAC TSR-2

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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)
Ulogu	Tactical Strike and Reconnaissance (TSR) Aircraft
National Origin	Ujedinjeno Kraljevstvo
Proizvođača	British Aircraft Corporation (Vickers-Armstrong & English Electric)
First Flight	27 Septembar 1964
Posada	2 (Pilot and Navigator/Weapon Systems Operator)
Dužina	27.13 m (89 ft)
Raspon krila	11.28 m (37 ft)
Visina	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.