Sopwith Triplane Typhoon

Boulton Paul P.92

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Contents

Type Description
Production Details

Type Description

  • P.92
  • Two-seat turret-armed day/night fighter to Specification F.11/37. It was to be of stressed-skin construction and have main undercarriage wheels that retracted backwards into the engine nacelles and wings (the wheels would rotate through 90 degrees to lie within the wing behind the nacelles). The engines would have underslung radiators. The Air Ministry recommended that leading-edge slots be fitted. The wing and Boulton Paul Type L conformal gun turret were designed as a single aerodynamic unit, the turret housing four 20 mm Hispano cannons in slots and had an all-around traverse. The turret was later redesigned to take an additional four belt-fed .303 Browning machine guns, fitted in two pairs outboard of the cannon, each pair in a single slot. The gunner's head protruded inside a small perspex blister set slightly back from the middle of the turret. The pilot sat in the nose with an excellent view forward but the view sideways was somewhat blocked off by the engines. The pilot and gunner were provided with separate hatches in the floor to bale out of in an emergency, the gunner could also jettison his blister and escape that way. The pilot's seat could be made to tip back and automatically release the bottom hatch so that he could slide down, head-first, out of the aircraft. Two prototypes were to be fitted with two 1,760 h.p. Rolls Royce Vulture II powerplants while the third would have the 2055 h.p. Napier Sabre I.

P.92 Specification
Span Length Height Wing Area Empty Wt Max AUW Cruise Speed* Maximum Speed* Endurance* Service Ceiling*
66 ft 3 in 55 ft 15 ft 3 in 709 sq ft 19100 lb 320 mph/ 278 kn 370 mph/ 322 kn 1.5hr 38000 ft
20.19 m 16.76 m 4.65 m 65.87 m2 8664 kg 515 km/h 595 km/h 11582 m
*Estimated

  • P.92/2
  • Single seat half scale aerodynamic test model for the P.92. To speed construction, it was to be made of wood and featured a fixed undercarriage with the two main wheels housed in streamlined "trouser" fairings. To better accommodate a normal-sized pilot, the cockpit and nose were made slightly larger and more bulbous in scale than the P92. Small windows were placed on either side of the fuselage, below the main cockpit canopy, to improve the view of the ground. Two 135 h.p. de Havilland Gipsy Major II powerplants.

P.92/2 Specification
Span Length Height Wing Area Empty Wt Max AUW Cruise Speed Maximum Speed Range Service Ceiling
33 ft 27 ft 6 in 7 ft 6 in 2778 lb 134 mph/ 116 kn 152 mph/ 132 kn
10.06 m 8.38 m 2.29 m 1260 kg 216 km/h 245 km/h


Production Details

P.92
Serial Range C/n Batch
Qty
Conv. Canc'd Notes
 3 aircraft ordered from Boulton Paul Aircraft Ltd, Wolverhampton, to Contract 708600/37. Not built.
 L9629, L9632, V9258        3  
Total Production 3
Serial Range C/n Batch
Qty
Conv. Canc'd Notes
 1 aircraft ordered from the Heston Aircraft Company Ltd, Heston, Middlesex, as the Heston JA.8, to Contract 19037/39. First flew spring 1941.
 V3142    1      
Total Production 1

Production Summary

All Aircraft By Type
Type Built New Conv Canc'd Total
 P.92 3 3
 P.92/2 1 1
1 (0) 3

Production References

  1. Boulton Paul Aircraft Since 1915,, Alec Brew (Putnam, 1993)
  2. https://dingeraviation.net/bpp100/bpp92.html

Page Revision History

Revised at Version 2.0.0
  • Added Type Description and Specification details.