The BAC Jet Provost was a British jet trainer aircraft used by the Royal Air Force from 1955 to 1993. Hunting Percival began design studies in early 1951 as a private venture and developed it from the piston-engined Percival Provost, deliberately reusing the Provost tail surfaces, main planes and main undercarriage legs to reach a prototype quickly. The prototype XD674 first flew from Luton Airport on 26 June 1954, and the type was later produced by the British Aircraft Corporation after Hunting became part of it. It is an all-metal, stressed-skin, side-by-side two-seater with a single Armstrong Siddeley Viper turbojet, and Flight International called it the first ab initio jet trainer standardised by any air force. The T3 entered service in 1959, the T4 and the pressurised T5 followed, and armed export versions went to Ceylon, Kuwait, Iraq, Sudan and others. It was withdrawn in the early 1990s in favour of the Short Tucano, and the design also led to the BAC Strikemaster.
Facts
Engine Class Top Speed (km/h) Maximum Mass (kg) EngineArmstrong Siddeley Viper Mk.102 / Mk.202 turbojet engine 1 Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source BAC Jet Provost (Wikipedia)
Of Make
Source BAC Jet Provost (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source BAC Jet Provost (Wikipedia)Lead, makerQuote, Lead, maker
It was originally developed by Hunting Percival from the earlier piston engine-powered Percival Provost basic trainer
Originated In
Also in Geography Atlas: where this subject originated.
Source BAC Jet Provost (Wikipedia)Lead, originQuote, Lead, origin
The BAC Jet Provost is a British jet trainer aircraft
Sources
1. BAC Jet Provost (Wikipedia)
Prototypes and evaluation, maiden flight
On 26 June 1954, the prototype XD674 conducted its maiden flight from the factory at Luton Airport
Lead, origin
The BAC Jet Provost is a British jet trainer aircraft
Specifications (Jet Provost T.5), powerplant
1 × Armstrong Siddeley Viper Mk.102 / Mk.202 turbojet engine
Specifications (Jet Provost T.5), powerplant, engine
1 × Armstrong Siddeley Viper Mk.102 / Mk.202 turbojet engine, 1,700 lbf (7.6 kN) thrust
Specifications (Jet Provost T.5), empty weight
Empty weight: 4,888 lb (2,217 kg)
Specifications (Jet Provost T.5), maximum take-off weight
Max takeoff weight: 9,200 lb (4,173 kg)
Specifications (Jet Provost T.5), speed
Maximum speed: 382 kn (440 mph, 707 km/h)
Operational service, withdrawal
The Jet Provost was withdrawn from RAF service during the early 1990s
Lead, maker
It was originally developed by Hunting Percival from the earlier piston engine-powered Percival Provost basic trainer
In Group: Military Trainer Aircraft, Lead, kind of craft
The BAC Jet Provost is a British jet trainer aircraft
Exemplifies: Aviation, Lead, kind of craft (mode)
The BAC Jet Provost is a British jet trainer aircraft
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