Vickers Type 161

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Type 161
Vickers 161.jpg
Role Interceptor fighter
National origin United Kingdom
Manufacturer Vickers Ltd.
First flight 21 January 1931
Number built 1

The Vickers Type 161 was an unusual 1930s pusher biplane interceptor, designed to attack aircraft from below with a single upward-angle large calibre gun. The aircraft flew well but the concept was abandoned and only one was built.


The Vickers 161[1] was designed in response to Air Ministry specification F.29/27. This called for an interceptor fighter operating as a stable gun platform for the COW 37 mm gun produced by the Coventry Ordnance Works (COW) that fired 23 oz (0.65 kg) shells. The gun was to be mounted at 45 degrees or more above the horizontal, so that the aircraft could fly below the target bomber or airship, and fire upwards into it. During World War II the Luftwaffe used a rather similar approach, named Schräge Musik. The specification also called for a top speed well in excess of a typical bomber's cruising speed and a good rate of climb.

Vickers' approach seems to have been influenced by their World War I experience with the Gunbus family. Like them, the Type 161[2] was a single-engined pusher biplane. The wings were of unequal span and parallel chord, mounted with heavy stagger and a large gap braced in two-bay fashion by streamlined I form, outward leaning interplane struts. Parallel booms, formed on each side by a pair of tubular members, converged from the top and bottom of the inner interplane struts onto the tail. Another pair of tubes joined the bottom of the interplane struts to the upper boom at midpoint. The tailplane had a wide span, extending past the booms; the fin and rudder were conventional and stiffened with lighter bracing to mid-boom. Flying surfaces were fabric covered.

Vickers 161 side view.jpg

The pilot and gun were housed in a metal monocoque nacelle mounted to the underside of the upper wing, leaving a gap below. The pilot's cockpit was offset to port with the gun to his right, its breech accessible. The Bristol Jupiter VIIF was installed with its cylinders in line with the rear edge of the upper wing, supported by two pairs of struts to the lower wing spars and driving a four-blade propeller. This had an unusual ring fairing that rotated with it and matched the engine cowling in diameter. Aft, and without a break, a fuselage-like fairing ran rearwards, narrowing to the tail. This structure was stabilized on each side by a pair of struts to the upper and lower booms. A split-axle undercarriage had legs to the fuselage and, rearwards, to the forward wing spar, with a strut between their upper joints.

The Type 161 flew[3] for the first time on 21 January 1931. Further flight trials produced some modifications, largely to improve yaw stability. The rudder was broadened and rounded at the top, and small fins were added above and below the tailplane at the boom mounting point. There were also alterations to the geometry and gearing of the elevator trim tabs: it has been suggested that the Type 161 may have been the first aircraft to have had inflight adjustable elevator trims.[4] In September 1931 it went to RAF Martlesham Heath for trials, where no serious problems emerged and pilot's reports were positive. The gun-firing tests went well, with no detriment to airframe or performance. Despite that, neither the Type 161 or its competitor the Westland C.O.W. Gun Fighter were ordered and no more was heard of the aerial COW gun.


Data from Andrews 1988 p.254

General characteristics

  • Crew: One
  • Length: 23 ft 6 in (7.16 m)
  • Wingspan: 32 ft 0 in (9.75 m)
  • Height: 12 ft 4 in (3.76 m)
  • Wing area: 270 ft2 (25.1 m2)
  • Empty weight: 2,318 lb (1,051 kg)
  • Gross weight: 3,350 lb (1,520 kg)
  • Powerplant: 1 × Bristol Jupiter VIIF 9-cylinder radial, 530 hp (395 kW)


  • Maximum speed: (at 10,000 ft, 3,048 m) 185 mph (298 km/h)
  • Rate of climb: (to 10,000 ft, 3,048 m) ft/min (8.76 m/s)


  • 1× 37 mm (1.46 in) COW automatic gun
  • See also

    Aircraft of comparable role, configuration and era


    1. ^ Andrews & Morgan 1988, pp. 242–6, 254, 515
    2. ^ Andrews & Morgan 1988, pp. 242–5
    3. ^ Andrews & Morgan 1988, pp. 243–6, 254
    4. ^ Andrews & Morgan 1988, pp. 245


    • Andrews, C. F.; Morgan, E. B. (1988). Vickers Aircraft since 1908 (2nd ed.). London: Putnam. ISBN 0-85177-815-1.
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