Airspeed Cambridge

Airspeed AS.45 Cambridge

Overview

The Airspeed AS.45 Cambridge was a British advanced trainer aircraft developed during the Second World War by Airspeed Limited.

Only two prototypes were built, and the type never entered production due to performance shortcomings and lack of wartime necessity.

Development History

Origins

Designed in response to Air Ministry Specification T.4/39, which sought a single‑engine advanced trainer to supplement or replace existing types like the Miles Master and North American Harvard.

The aircraft was given the provisional service name Cambridge.

Design Features

Low‑wing monoplane of composite construction:

Steel‑tube fuselage

Wooden wings and tail, plywood‑skinned

Tandem seating for pilot and instructor in an enclosed cockpit, each with:

A normal door

A dedicated emergency exit

Retractable tailwheel undercarriage.

Powered by a 730 hp Bristol Mercury VIII radial engine driving a three‑bladed propeller.

First Flight

The first prototype flew on 19 February 1941.

Testing & Evaluation

Flight testing revealed two major deficiencies:

Insufficient maximum speed

Poor low-speed handling characteristics

These issues were never corrected, for two reasons:

The RAF already had adequate supplies of advanced trainers (Masters and Harvards).

Airspeed was heavily committed to more strategically important aircraft:

Airspeed Horsa troop glider

Airspeed Oxford trainer/transport

As a result, the Cambridge programme was quietly discontinued after the two prototypes.

Specifications

Crew

2

Length

36 ft 1 in (11.00 m)

Wingspan

42 ft 0 in (12.80 m)

Height

11 ft 6 in (3.51 m)

Wing area

290 sq ft (27 m²)

Powerplant

1 × Bristol Mercury VIII radial engine, 2-blade,

730 hp (540 kW)

Performance

Maximum speed

237 mph (381 km/h, 206 kn)

Range

680 mi (1,090 km, 590 nmi)

Service ceiling

24,800 ft (7,600 m)

Rate of climb

1,200 ft/min (6.1 m/s).

Digital Artworks by Peter Coletti.

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