The Handley Page Basic Trainer, designated H.P.R.2, was a British training aircraft of the 1940s and early 1950s: a single-engine, low-wing monoplane with a fixed tailwheel undercarriage and a three-bladed constant-speed propeller. Handley Page Reading Ltd designed it to answer Air Ministry Specification T16/48, which called for a trainer to replace the ageing Percival Prentice, and it was powered by a seven-cylinder Armstrong Siddeley Cheetah radial engine of 420 horsepower. It first flew in May 1950, and two prototypes were built and flown. Trials showed it to be a trickier and less forgiving aeroplane than its rival, the Percival P.56, and although the company believed it could be improved, the Air Ministry chose the P.56 for production as the Provost. No orders followed, so the type never entered service and remains a footnote in the story of the post-war British trainer competition.
Facts
Engine Class Top Speed (km/h) Maximum Mass (kg) EngineArmstrong Siddeley Cheetah XVIII 1 Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Handley Page Basic Trainer (Wikipedia)
Of Make
Source Handley Page Basic Trainer (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Handley Page Basic Trainer (Wikipedia)DevelopmentQuote, Development
The H.P.R.2 was developed by Handley Page Reading Ltd as a basic trainer
Originated In
Also in Geography Atlas: where this subject originated.
Source Handley Page Basic Trainer (Wikipedia)LeadQuote, Lead
The Handley Page Basic Trainer (H.P.R.2) was a British training aircraft of the 1940s.
Sources
1. Handley Page Basic Trainer (Wikipedia)
Development, first flight
The Basic Trainer first flew in May 1950.
Lead
The Handley Page Basic Trainer (H.P.R.2) was a British training aircraft of the 1940s.
Specifications, powerplant
Powerplant: 1 × Armstrong Siddeley Cheetah XVIII 7-cyl. air-cooled radial piston engine, 420 hp (310 kW)
Specifications, engine type
Powerplant: 1 × Armstrong Siddeley Cheetah XVIII 7-cyl. air-cooled radial piston engine, 420 hp (310 kW)
Specifications, power
Powerplant: 1 × Armstrong Siddeley Cheetah XVIII 7-cyl. air-cooled radial piston engine, 420 hp (310 kW)
Specifications, takeoff weight
Max takeoff weight: 4,421 lb (2,005 kg)
Specifications, speed
Maximum speed: 173 mph (278 km/h, 150 kn) at 2,500 ft (760 m)
Development, prototypes
Two prototypes (WE496 c/n HPR.142 and WE505 c/n HPR.143) were built and flown but no orders resulted.
Development, outcome
Two prototypes (WE496 c/n HPR.142 and WE505 c/n HPR.143) were built and flown but no orders resulted.
Development
The H.P.R.2 was developed by Handley Page Reading Ltd as a basic trainer
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