Westland Wasp

Summary

Category Military Helicopters
Origin country 🇬🇧 United Kingdom
ManufacturerWestland
First flight28 October 1962
Year introduced1964
Number produced133 units

Technical specifications

Version: Wasp HAS.1
Crew1 pilot, 1 Aircrewman
Operational range487 km (303 mi)
Maximum speed 193 km/h (120 mph)
Wing area75.9 m² (816.9 sqft)
Wingspan9.8 m (32.3 ft)
Height2.7 m (8.9 ft)
Length12.3 m (40.3 ft)
Service ceiling3,700 m (12,139 ft)
Empty weight1,566 kg (3,452 lbs)
Max. takeoff weight2,495 kg (5,501 lbs)
Climb rate7.3 m/s (24.0 ft/s)
Powerplant1 x Rolls-Royce Nimbus 103 delivering 530 kW each

Current operating countries

No country is operating the Wasp in 2026.

All operators

🇧🇷 Brazil • 🇬🇧 United Kingdom • 🇮🇩 Indonesia • 🇲🇾 Malaysia • 🇳🇱 Netherlands • 🇳🇿 New Zealand • 🇿🇦 South Africa

Armament

Missiles payload:

Bombs payload:

  • Unguided Bomb Mk 11 depth charge
  • Nuclear WE.177 Nuclear Depth Bomb

Westland Wasp Helicopter profile drawing

Description

The Westland Wasp was a British shipboard anti-submarine helicopter developed by Westland Helicopters from the Saunders-Roe P.531 programme and based on the piston-engined Saunders-Roe Skeeter. It was designed to meet a Royal Navy requirement for a Manned Torpedo-Carrying Helicopter (MATCH). The first prototype Saro P.531 flew on 20 July 1958, and two pre-production aircraft flew on 28 October 1962. A total of 133 aircraft were produced, including 98 for the Royal Navy.

The Wasp was powered by a Rolls-Royce Nimbus 103 turboshaft engine de-rated to 710 shp. Lacking onboard sonar, the helicopter relied on external targeting data to deliver weapons. To operate from pitching flightdecks, it featured a four-wheeled castering undercarriage, negative rotor pitch for deck adhesion, and foldable main rotor blades and tail boom. Additional features included a starboard winch, an under-fuselage cargo release unit, floor fuel tanks, emergency floats, and a cockpit-roof aimer's sight. The cabin accommodated a pilot, an aircrewman, and up to three passengers or a single stretcher.

The aircraft carried two Mk 44 torpedoes, one Mk 46 torpedo, two Mk 11 depth charges, or a WE.177 nuclear depth bomb. For surface targets, it was armed with four Nord SS.11 or two AS.12 wire-guided missiles, an L7 GPMG, flares, and smoke or flame floats.

The Royal Navy introduced the Wasp in 1964 and retired the type in 1988. On 25 April 1982, three Wasps launched from HMS Plymouth and HMS Endurance attacked the Argentinian submarine ARA Santa Fe with AS.12 missiles in South Georgia, disabling the vessel. Export operators included the Netherlands, which flew 12 AH-12As from 1966 to 1981; New Zealand, which operated 19 aircraft from 1966 to 1998; and South Africa, which received ten aircraft in 1963 and six of an ordered eight from 1973, retiring them in 1990. Brazil operated the type from destroyers and frigates, Malaysia operated Wasps from 1988 to 1998, and Indonesia operated refurbished ex-Dutch aircraft until 1998.

Main Variants

  • Sea Scout HAS.1: The original Royal Navy designation for the helicopter.

  • Wasp HAS.1: The standard shipboard anti-submarine warfare variant operated by the Royal Navy.

  • UH-2/UH-2A: The Brazilian Navy designations for the aircraft, with the UH-2 originally designated SH-2.

Frequently Asked Questions

What type of aircraft is the Wasp?
The Westland Wasp is a military helicopters aircraft developed by Westland and entered service in 1964.
What is the maximum speed of the Wasp?
The Westland Wasp has a maximum speed of 193 km/h (119 mph).
What is the range of the Wasp?
The Westland Wasp has an operational range of 487 km (302 miles). This range can vary based on payload, altitude, and mission profile.
When did the Wasp first fly?
The Westland Wasp made its first flight on October 28, 1962. It entered operational service in 1964.
How many Wasp have been built?
Approximately 133 units of the Westland Wasp have been produced since it entered service in 1964.
What is the service ceiling of the Wasp?
The Westland Wasp has a service ceiling of 3,700 meters (12,139 feet). This is the maximum altitude at which the aircraft can maintain controlled flight.
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