The Bristol Type 148 was a two seat, single engine low wing monoplane built in 1937 to an Air Ministry specification, A.39/34, for an army cooperation aircraft meant to replace the Hawker Audax and Hector. Following the layout of the Types 133 and 146, it had stressed skin wings of constant chord, an all monocoque fuselage, split flaps and connected wingtip slots for handling at low speed, and a pilot and observer in tandem cockpits under a continuous canopy. The intended engine was the Bristol Perseus, but it made its first flight on 15 October 1937 with a Mercury IX. It lost the competition to the Westland Lysander and did not progress past the two prototypes built.
Facts
Engine Class Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Bristol Type 148 (Wikipedia)
Of Make
Source Bristol Type 148 (Wikipedia)
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Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Bristol Type 148 (Wikipedia)LeadQuote, Lead
The Bristol Type 148 was a two-seat, single-engine low-wing monoplane built in 1937 to an Air Ministry specification for an army cooperation aircraft.
Sources
1. Bristol Type 148 (Wikipedia)
Lead
The Bristol Type 148 was a two-seat, single-engine low-wing monoplane built in 1937 to an Air Ministry specification for an army cooperation aircraft.
Lead and development
the aircraft made its first flight on 15 October 1937 with a Mercury IX
Engine
Powerplant: 1 × Bristol Taurus II 14-cylinder two-row sleeve-valve radial , 1,050 hp (783 kW)
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