Safat 02

SAFAT Aviation Group
http://safatavia.com/our-products/safat-02/

Safat 02

SAFAT02

SAFAT 02_1

and stationary objects, increase situational awareness
The system adds many feature to helicopter such as:-
Support and coordinate the operators’ interaction when engaging targets;
Provide the crew with enhanced flight and situational awareness
Support extensive flight management capabilities and a full range of navigation and flight planning features together with simple route and flight plan creation and modification procedures.
Provide manual and directed modes of flight control;
Increase flight safety;
Provide day and night helicopter operations;
Provide complete flight recording including the engagement results;
Assure flight management information for safe returning and landing

Specifications

 

ESTIMATED WEIGHTS:

Maximum takeoff weight 650 kg
Empty helicopter weight 380 kg

FLIGHT CHARACTERISTICS

Maximum ground airspeed 186 km/h
Ground cruising airspeed 160 km/h
Static ceiling for hovering out of ground effect (gross weight) 1000 m
Flight duration at Н=0 – 1000 m 3 hrs

GEOMETRICAL DIMENSIONS

Cockpit  Internal dimensions:

length

width

height

1.52 m

1.4 m

1.2 mUndercarriage

length

distance between skids

1.82 m

1.65 mTotal length :

@ Max main rotor blades

@ Max cabin point

8 m

5.8 mMain rotor Diameter6.8 m

POWER PLANT INFORMATION

One horizontal piston four-cylinder four-act liquid-cooled engine Subaru EJ-25. Japanese Subaru, EJ-25 model
Engine power 156 horsepower (115 kW)
Max Crank shaft speed 5600  rpm
Approved Fuel 72 Liters capacity, 19.1 US Gallon or 16 UK Gallon

Unleaded Automotive Gasoline, Octane 95Approved Oil5W 50, Universal motor Oil for Gasoline engine class SL (API min)Oil system servicing4.2 to 4.5 litersCooling system servicing10 litersFuel Consumption24 to 32 L/H

SAFAT0222

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