Turbojet engine
Locust H220R
Locust H220R is a high-performance turbojet engine designed for target unmanned aircraft and high-speed UAVs, combining compact dimensions, high thrust and robust construction.
Availability and configuration on request
PRODUCT OVERVIEW
Locust H220R
Locust H220R is a high-performance turbojet engine designed for target unmanned aircraft and high-speed UAVs, combining compact dimensions, high thrust and robust construction.
KEY ADVANTAGES
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High thrust in its class
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Compact and lightweight
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Fuel-efficient operation
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Modular construction
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Designed for demanding conditions
APPLICATIONS
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Light UAVs and drones
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Aerial targets
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Robotic systems
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Ground and research platforms
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Mobile reconnaissance systems
TECHNICAL SPECIFICATIONS
Specifications
Maximum thrust (5 min)
220 lb / 100 kgf / 980 N
Continuous thrust
187 lb / 85 kgf / 830 N
Engine weight
30 lb / 14.5 kg
Maximum RPM
75,000 rpm
Diameter
8.15 in / 207 mm
Length
21.4 in / 544 mm
Compression ratio
6 : 1
28 V DC generator
1 kW
Bearing life
100 h
Fuel consumption at max thrust
2.15 L/min
Cruise fuel consumption
1.32 L/min
REQUEST
Order Locust H220R
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