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 off 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                                      Version for driving

     forward-mounted propeller (puller)                         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:

SOME HISTORY FACTS





10,000

Tonnes of iron
Shot at Siege of Sebastopol during Crimean War





144,000

Revolutions per minute
Does a bullet fired from Lee Enfield rifle, as used in both world wars





2,000

Women
The Nizam of Hyderabad raised in 1975 for his war against the Marathas





130,000

Meters
Is an effective range of Big Bertha, the World War I howitzer


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Contact Information

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State Foreign Trade Enterprise “SpetsTechnoExport” is a fully state-run entity incorporated by the Government of Ukraine in 1998 for export-import activities at foreign armaments markets.

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