Malkara (missile)

Summary

The Malkara (from an Aboriginal word for "shield") was one of the earliest guided anti-tank missiles (ATGMs). It was jointly developed by Australia and the United Kingdom between 1951 and 1954, and was in service from 1958 until gradually replaced by the Vickers Vigilant missile in the late 1960s. It was intended to be light enough to deploy with airborne forces, yet powerful enough to knock out any tank then in service. The basic form was later adapted for the short-range surface-to-air role as the Seacat and influenced the development of the Ikara.

Malkara
Malkara on display at the Tank Museum, Bovington.
TypeAnti-tank guided missile
Place of originAustralia,
United Kingdom
Service history
In service1958 to 1960s
Used byUnited Kingdom
Production history
DesignerRoyal Aircraft Establishment/Aeronautical Research Laboratory
Designed1954
ManufacturerGovernment Aircraft Factories/Fairey Engineering Ltd
Produced1958-1964
No. built1,000
Variantsnone
Specifications
Mass93.5 kg (206 lb)
Length1.9 m (6 ft 3 in)
Diameter203 mm (8.0 in)
Wingspan80 cm (2 ft 7 in)
Warhead26 kg (57 lb) HESH
Detonation
mechanism
impact

Enginesolid rocket
Operational
range
4,000 metres (2.5 mi)
Guidance
system
wire guided line of sight
Steering
system
control surfaces
Launch
platform
Vehicle

Development and operations edit

Design was principally undertaken at the Australian Government Aeronautical Research Laboratory, and this phase was also one of the first examples of computer simulation in engineering design. Development testing was carried out at Woomera Prohibited Area, and approval testing at the tank training range at Lulworth Cove, Dorset. Although testing at Dorset apparently achieved an impressive 90% Pkill, in service the missiles were not considered a great success, due to three principal failures:

  • They were considered too heavy. As they were too heavy for manpacking, they could only be operated from their specialist vehicles, reducing flexibility; and
  • Accuracy achieved in practice was poor. This may have been because the awkward control system required a lot of practice. Malkara had a training simulator integrated with the launch interface equipment. In their memoirs, some operators state that they only fired one missile in their careers.
  • Finally, their speed was low, taking almost 30 seconds to reach maximum range.
 
Malkara-equipped Humber Hornet vehicle

However, lessons learned from the Malkara project led to improvements in later programs. In addition, the basic airframe and expertise were directly used in the development of the Ikara anti-submarine missile and the Sea Cat naval surface-to-air missile.

Malkara was unusual among anti-tank missiles in that it had a High-explosive squash head (HESH), also known as High Explosive Plastic (HEP), warhead instead of the more usual shaped charge HEAT (High Explosive Anti Tank) warhead. The United Kingdom always showed interest for HESH, the main explosive-based anti-tank ammunition in British use including contemporary tanks like the Centurion. A 26/27 kg anti-tank warhead was well above the average, but Malkara had a calibre of 203 mm (8.0 in).

Operators edit

  United Kingdom

Specifications edit

 
  • Length: 1.9 m (6.2 ft)
  • Diameter: 200 mm (7.9 in)
  • Wingspan: 800 mm (2.6 ft)
  • Range: 4,000 m (4,400 yd)
  • Propulsion: Dual thrust solid rocket
  • Speed: 146.19 m/s (327 mph) - low-subsonic, 28 sec to 4 km max range
  • Overall weight: 93.5 kg (206 lb)
  • Warhead: 26 kg (57 lb) HESH
  • Guidance: Wire guided MCLOS, using a thumb joystick and visual observation of two flares on the wings.
  • Number built: 1,000

See also edit

References edit

Sources edit

  • War Machine encyclopedia, Aerospace Publishing Ltd., pag. 253 (in Italian version printed by De Agostini, 1984).
  • Rockets and Missiles - John W. R. Taylor - Hippo Books No 8 - Hamlyn, 1971 - ISBN 0-600-37528-5