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UAV · MALE UAV demonstrator

Mantis

BAE Systems · United Kingdom

Twin-turboprop MALE UAV advanced concept technology demonstrator developed for the UK MoD for ISR and potential strike. Maiden flight 2009 at Woomera, Australia.

CountryUnited Kingdom
SubcategoryFixed-wing
SubtypeMALE UAV demonstrator
RoleISR/strike
ClassMALE
ClassificationMALE UAV
MissionISR, strike
Notable partnersRolls-Royce, Selex Galileo, GE Aviation
MTOW (kg)9000
OperatorsUnited Kingdom (MoD trials)
Frame typeFixed-wing
Length (m)19.8
PropulsionTurboprop
Wingspan (m)20
Combat-provenNo
Launch methodRunway takeoff
Autonomy levelFully autonomous
Endurance (min)1800
Recovery methodRunway landing
Year introduced2009
Max speed (km/h)556
Production statusPrototype
Service ceiling (m)16764
Airframe / lift typeFixed-wing
Control / autonomy levelFully autonomous (human-off-the-loop, AI-navigated)
DomainAerial (UAV/UAS)
Mission / use case – civilResearch
Mission / use case – militaryArmed UCAV, ISR
Origin / supply chainMilitary-grade
PropulsionTurbine / jet
Range / enduranceLong endurance (>24 hrs)
Signature / detectabilityRCS – large
Speed regimeHigh-speed / jet (>400 km/h)
Strike depth / operational roleMissile-drone / cruise-drone hybrid (jet-powered, e.g. Palianytsia, Peklo), Recon-strike complex (ISR + strike paired, e.g. Mavic + FPV, Orlan + Lancet)
Threat vectorSurveillance / reconnaissance
Weight / classClass III – MALE (>600 kg), FAA >25 kg (Part 137 / waiver)
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In the news 1

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Mantis
Robert Frola · GFDL · via Wikimedia Commons
Review-stage catalogue data — specs corroborated from manufacturer and secondary sources; not for procurement decisions. Source: www.baesystems.com