Engines For Unmanned Airial Vehicles

PISTON, TURBOPROP AND TURBOSHAFT ENGINES

TURBOJET AND TURBOFAN ENGINES

PISTON ENGINES
Version
Qty of cylinders
Dislplacement,  cu. cm
Power,                
kW/rpm
SFC, kg/kW•h
SLS, ISA
Max. power
Cruise power
Max. power
Cruise power
МS-75DLА
1
74.5
4.3 / 10,000
3.7 / 7,600
0.530
0.550
МS-150DLА
2
149
8 / 9,000
7 / 7,500
0.500
0.480
МS-300DLА
4
298
16 / 8,500
14 / 7,000
0.400
0.420
МS-640DLА
2
637
40 / 5,800
26 / 4,000
0.350
0.380
 
The engines can power the UAVs of similar types:
Schiebel Camcopter

DENEL AS Seeker II

Tactical Aerospace Group M-65

AI-450

Turboshaft engine with single-shaft gas generator, single-stage centrifugal-flow 
compressor, power turbine and built-in reduction gear

SPECIFICATIONS (If operated on piloted aircraft)   
Emergency power rating 
(SLS, ISA+15°C): 
Power, kW (hp) .................................................404.5(550) 
Takeoff power rating 
(SLS, ISA+15°C): 
Power, kW (hp) ................................................... 342(465) 
Specific fuel consumption, 
kg/kW•h (kg/hp•h) ...................................... 0.353 (0.260) 
Maximum continuous power rating 
(SLS, ISA+15°C): 
Power, kW (hp) .................................................. 294 (400) 
Maximum cruise power 
(SLS, ISA+15°C): 
Power, kW (hp) ................................................... 221(300) 
Specific fuel consumption, 
kg/kW•h (kg/hp•h) ...................................... 0.404 (0.297) 
Dry weight, kg ............................................................ 103

The engine can power the UAVs of similar types:
Northrop Grumman RQ-8A Fire Scout

Mi-34BP

AI-450S - Engine
AI-450 engine turboprop modifications for forward-mounted or aft propeller
SPECIFICATIONS*
 
АI-450S  
АI-450S-2  
АI-450S-3  
Take of f power rating (SLS , ISA+15°C):  
 
 
 
Power, shp (kW)
400 (294)
630 (463)
1,000 (735)
Specific fuel consumption,
kg/shp h (kg/kW•h)
0.292 (0.395)
0.272 (0.370)
0.258 (0.350)
Maximum continuous power rating (SLS, ISA):  
 
 
 
Power, shp (kW)
350 (257)
560 (411)
880 (647)**
Maximum cruise power rating
(H=3,000 m, M=0,2, ISA):
 
 
 
Power, shp (kW)
278 (204)
450 (331)
593 (436)
Specific fuel consumption,
kg/shp•h (kg/kW•h)
0.290 (0.394)
0.262 (0.356)
0.260 (0.353)**
Dry weight, kg
123
160
175
 
* When operating the manned aerial vehicle
** It remains up to +10°C under ISA
Note: All specifications given are only for engines operated on piloted aircraft
 
The engine can power the UAVs of similar type:
AHK Suhoi ZOND-3

Version for driving forward-mounted propeller (puller)

Version for driving aft propeller (pusher)

TV3-117 - Engine 

Family of turboprop and turboshaft engines with single-shaft gas-generator and free turbine

Possible version of UAV power plant with pusher propeller

The engine can power the UAV of similar type:



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