Handley Page Victor
Summary
| Category | Bombers |
| Origin country | 🇬🇧 United Kingdom |
| Manufacturer | Handley Page |
| First flight | 24 December 1952 |
| Year introduced | 1958 |
| Number produced | 86 units |
Technical specifications
| Version: Victor B.1 | |
|---|---|
| Crew | 5 |
| Operational range | 9,662 km (6,004 mi) |
| Maximum speed | 1009 km/h (627 mph) |
| Wing area | 223.5 m² (2405.7 sqft) |
| Wingspan | 34 m (111.5 ft) |
| Height | 8.6 m (28.1 ft) |
| Length | 35.0 m (114.9 ft) |
| Service ceiling | 17,000 m (55,774 ft) |
| Empty weight | 40,383 kg (89,029 lbs) |
| Max. takeoff weight | 92,986 kg (204,999 lbs) |
| Powerplant | 4 x Armstrong Siddeley A.S.Sa.7 Sapphire turbojet delivering 12 kN each |
Current operating countries
All operators
Armament
Missiles payload:
- Air-to-Surface Blue Steel
- Air-to-Ground AGM-48 Skybolt
Bombs payload:
- Nuclear Blue Danube
- Nuclear Yellow Sun
- Nuclear Mark 5
- Nuclear Red Beard
- Unguided Bomb Grand Slam
- Unguided Bomb Tallboy
- Unguided Bomb 1,000 lb bomb
- Unguided Bomb 2,000 lb sea mine
Description
The Handley Page Victor was a jet-powered strategic bomber produced for the Royal Air Force as the third and final V-bomber. It originated from Ministry of Supply Specification B.35/46, which required an aircraft capable of carrying a 10,000 lb weapon to a target 1,500 nautical miles away at speeds of 500 knots. The HP.80 prototype first flew on 24 December 1952, and the aircraft entered service in 1958. Production included 50 B.1 and 34 B.2 aircraft. The Victor remained in operational service until 15 October 1993, at which point it was replaced by Vickers VC10 and Lockheed Tristar tankers.
The aircraft featured a crescent-shaped swept wing with sweep and chord decreasing in three steps toward the tips to maintain a constant critical Mach number. Powerplants consisted of four engines buried in the wing roots; the B.1 used Armstrong Siddeley Sapphire ASSa.7 turbojets, while the B.2 utilized Rolls-Royce Conway turbofans. The Victor utilized a T-tail configuration and a pressurized cabin for a five-man crew. Avionics included the Navigational and Bombing System (NBS), H2S radar, and Green Satin radar. Defensive systems comprised an electronic countermeasures (ECM) suite and the Red Steer tail warning radar. The B.2 variant introduced ram air turbines to provide emergency electrical power in the event of engine failure.
The internal bomb bay was designed for a 10,000 lb nuclear weapon, such as Blue Danube or Yellow Sun, or tactical weapons like Red Beard and US-owned Mark 5 bombs. Conventional payloads included up to forty-eight 1,000 lb bombs, one 22,000 lb Grand Slam, or two 12,000 lb Tallboy earthquake bombs. The B.2RS variant was modified to carry the Blue Steel standoff nuclear missile.
Initially part of the UK’s nuclear deterrent, the Victor shifted to a low-level penetration profile in the 1960s. Fatigue cracks discovered in 1968 led to the type's retirement from the nuclear mission. In 1964, B.1As deployed to Singapore during the Borneo conflict as a conventional deterrent. Many airframes were subsequently converted for strategic reconnaissance (SR.2) or as aerial refueling tankers. During the 1982 Falklands War, Victor tankers supported Vulcan bombers during the Black Buck raids, which were the world's longest-distance bombing missions at that time. Eight K.2 tankers supported coalition aircraft during the 1991 Gulf War.
Main Variants
- Victor B.1: Initial production strategic bomber powered by Sapphire turbojet engines.
- Victor B.1A: Updated B.1 variant featuring Red Steer tail warning radar and an electronic countermeasures suite.
- Victor B.2: Improved bomber version with Rolls-Royce Conway turbofans, increased wingspan, and enlarged intakes.
- Victor B.2RS: Missile carrier variant modified to carry the Blue Steel standoff nuclear weapon and equipped with RCo.17 engines.
- Victor K.2: Dedicated aerial refueling tanker converted from B.2 and SR.2 airframes with a 91,000 lb fuel capacity.