Bristol Type 133

Ad: This forum contains affiliate links to products on Amazon and eBay. More information in Terms and rules

johnbr

2nd Lieutenant
5,591
5,161
Jun 23, 2006
London Ontario Canada
Bristol Type 133 | BAE Systems | International The Bristol Type 133 after its first flight, showing open cockpit and full span ailerons/flaps. A side view of the Type 133 R-10 fitted with an enclosed cockpit canopy. The Bristol Type 133 looked elegant in flight, like a precursor of the Vought Corsair. The promising Bristol Type 133 came to a sad end during its spinning trials.
Bristol Type 133 1.jpg
Bristol Type 133  2.jpg
Bristol Type 133  3.jpg
Bristol Type 133  4.jpg
 
Specification PowerplantOne 640 hp Bristol Mercury VIS.2 Span39 ft 0 inMaximum Weight4,738 lbCapacity and armamentPilot only; four forward firing Vickers machine gunsMaximum Speed260 mph equipped
Variants
Single example only, flown marked as R-10
The Bristol 133 was a prototype single-seat monoplane fitted with a single engine and retractable undercarriage. It was the company's second offering (after the Goshawk-powered Type 123 biplane) against Specification F.7/30 for a four-gun day and night fighter.

The type used a 620hp Bristol Mercury VI engine and was of inverted gull-wing configuration with fairings for the retractable main wheels mounted from the 'knuckle' of the wing.

The Type 133 (R-10) was first flown by Cyril Unwins with an open cockpit on 8th June 1934 - a cockpit enclosure being subsequently fitted. Other striking features included a monocoque rear fuselage and (initially) full span ailerons that could be symmetrically drooped as flaps.
The aircraft later reverted to more conventional ailerons with split flaps under the centre-section. The clean engine cowling featured a long-chord Townend-ring cowling, with an integral exhaust collector-ring.
Sadly the Type 133 did not reach Martlesham Heath for official trials, being lost in a spinning accident on 8th March 1935 with the pilot escaping by parachute. The problem occurred whilst spinning with the undercarriage down. It was evident that the aircraft was in a flat spin and it had very little forward speed when it reached the ground.
 

Users who are viewing this thread

Back