Airspeed AS.45 Cambridge

1st Flight 1941

Military Users- Prototypes Only

Airspeed AS.45 Cambridge

 

The AS.45 was designed in response to Air Ministry Specification T.4/39 for a single engine trainer.

It was a low-wing monoplane of composite construction with a single piston engine and a tail wheel-type, retractable undercarriage.

Airspeed AS.45 Cambridge

The first of two prototypes flew on 19 February 1941.

Testing showed deficiencies in both maximum speed and low-speed flight characteristics.

There was no attempt to rectify these shortcomings, partly because there was no shortage of advanced trainers thanks to plentiful supplies of Masters and Harvards and partly because of the importance of Airspeed’s other products, the Horsa and Oxford.

Airspeed AS.45 Cambridge

Specifications-

Crew: 2

Length: 36 ft 1 in (11 m)

Wingspan: 42 ft 0 in (12.80 m)

Height: 11 ft 6 in (3.51 m)

Wing area: 290 sq ft (26.94 m2)

Airspeed AS.45 Cambridge

Power plant: 1 × Bristol Mercury VIII radial engine 2-blade, 730 hp (544 kW)

Performance

Maximum speed: 237 mph (381 km/h, 206 kn)

Range: 680 mi (1,094 km, 590 nmi)

Service ceiling: 24,800 ft (7,560 m)

Airspeed AS.45 Cambridge

Credits-

Airspeed Aircraft since 1931-H.A. Taylor.

Aircraft of the Royal Air Force 1918-58-Owen Thetford.

Wikipedia.

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