BAE Systems Mantis

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Mantis
BAEMantisMockUp.JPG
Mock up of BAE Systems Mantis at Farnborough Airshow 2008
Role UAV demonstrator
Manufacturer BAE Systems Military Air & Information
First flight 21 October 2009[1]
Status Test program active
Primary user United Kingdom
Produced 1

The BAE Systems Mantis Unmanned Autonomous System Advanced Concept Technology Demonstrator is a British demonstrator programme for Unmanned Combat Air Vehicle (UCAV) technology. The Mantis is a twin-engine, turboprop-powered UCAV with a wingspan of approximately 22 m, broadly comparable to the MQ-9 Reaper. Other partners involved in Phase 1 of the Mantis programme include the UK Ministry of Defence, Rolls-Royce, QinetiQ, GE Aviation, L-3 Wescam, Meggitt and Lola.

Design and development

Description board for Mantis at Farnborough Airshow 2008

Development of the Mantis started in late 2007, a mockup being revealed at the 2008 Farnborough International Air Show. The Phase 1 Mantis vehicle is powered by two Rolls-Royce Model 250 turboprop engines, although this is likely to change in later variants. The Mantis is intended to have at least 24-hour operational endurance and is an autonomous vehicle, able to pilot itself and to plot its own course, communicating with personnel on the ground regarding its observations.[2]

Phase 1 is intended to demonstrate BAE Systems' rapid prototyping capabilities and will focus on the evaluation of autonomous control systems. Later phases may evaluate civilian applications, armed variants and sensor packages.

The large dome on the front, reminiscent of a pilot's canopy, actually contains an upward facing satellite communications system.

The prototype first flew on 21 October 2009 at Woomera Test Range in South Australia.[1]

In 2013 the Mantis was flight tested in the United Kingdom.[3] It is being used as the basis for the new BAE/Dassault Telemos UAV.[4]

Specifications

Data from FlightGlobal,[5] Rolls-Royce[6]

General characteristics

  • Crew: none (UAV)
  • Length: 19.8 m (65 ft 0 in)
  • Empty weight: 1,000 kg (2,205 lb)
  • Max takeoff weight: 9,000 kg (19,842 lb)
  • Powerplant: 2 × Rolls-Royce M250B-17 turboprop, 280 kW (380 shp) each

Performance

  • Maximum speed: 556 km/h; 345 mph (300 kn)
  • Cruise speed: 370 km/h; 230 mph (200 kn)
  • Endurance: 30 hours

Armament

  • Hardpoints: Six

Avionics

See also

Related development
Related lists

References

  1. 1.0 1.1 Lua error in package.lua at line 80: module 'strict' not found.
  2. Mantis, gallery of future drones, Popular Science, March 2010.
  3. [1], BAE Systems Newsroom, 9 July 2012.
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External links