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Handley Page Basic Trainer

Military Aircraft

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
Year
1950 1
Engine Class
Piston 1
Status
Prototype 1
Power (kW)
313 1
Units Built
2 1
Top Speed (km/h)
278 1
Maximum Mass (kg)
2005 1
Engine
Armstrong Siddeley Cheetah XVIII 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
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)Development
Quote, 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)Lead
Quote, 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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