Aerokopter

Manufacturer:

Aerokopter

Country:

Ukraine

Commercial designation:

Sanka

Technical designation:

AK1-3

Version, Variant:

Type:

Conventional

Currently produced:

Y

Typical missions:

Civil

Flight conditions:

VFR

First flight:

2001

Landing system:

skids

Blades number:

3

Tail blades number:

2

MTOW with external loads:

650 kg

1433.25 lbs

MTOW with only internal loading:

650 kg

1433.25 lbs

Empty weight:

380 kg

837.9 lbs

External payload:

0 kg

0 lbs

Internal payload:

270 kg

595.35 lbs

Standard fuel tank:

58 kg

127.89 lbs

with optionnal external fuel tank:

0 kg

0 lbs

Cruise speed:

0 km/h

0 kt

Maximum cruise speed:

160 km/h

86.4 kt

Vne:

186 km/h

100.44 kt

Max negative g @ MTOW:

0.5 g

Max positive g @ MTOW:

2.5 g

Range with normal tanks:

450 km

243 nm

Max range with auxiliary external tanks:

0 km

0 nm

Max endurance @ min consumption speed:

03:00:00 h:min

Rate of climb @ SL:

9.2 m/s

1810.56 ft/min

Rate of climb @ SL @MTOW:

8 m/s

1574.4 ft/min

IGE max hovering altitude, MTOW:

0 m

0 ft

IGE max hovering altitude, empty:

0 m

0 ft

IGE max hovering altitude, ISA+20°C, MTOW:

0 m

0 ft

IGE max hovering altitude, ISA+20°C, empty:

0 m

0 ft

OGE max hovering altitude, MTOW:

1500 m

4920 ft

OGE max hovering altitude, empty:

2100 m

6888 ft

OGE max hovering altitude, ISA+20°C, MTOW:

0 m

0 ft

OGE max hovering altitude, ISA+20°C, empty:

0 m

0 ft

Service ceiling ISA, MTOW:

3000 m

9840 ft

Max operating altitude, empty weight:

0 m

0 ft

Highest use Temperature:

0 °C

0 °F

Lowest use Temperature:

0 °C

0 °F

APU in HC:

N

Engine manufacturer:

Subaru

Model:

EJ25

Engines quantity:

1

Powerplant category:

piston

Main rotor rotation speed:

540 rpm

Fuel consumption @ SL @ max continuous speed:

0 kg/kW/h

0 lbs/hp/h

Minimum consumption speed @ SL:

0 km/h

0 kt

Fuel consumption @ eco cruise speed @SL:

0 kg/h

0 lbs/h

Fuel consumption @ min consumption speed @ SL:

0 kg/h

0 lbs/h

Engines nominal power:

121 kW

164.439 hp

Transmission shaft max continuous power:

0 kW

0 hp

Transmission shaft max power:

0 kW

0 hp

Takeoff power 5 min:

121 kW

164.439 hp

OEI 30s power:

0 kW

0 hp

OEI 2min power:

0 kW

0 hp

OEI max continuous power :

0 kW

0 hp

OEI max continuous transmission power:

0 kW

0 hp

OEI 30 sec transmission power:

0 kW

0 hp

OEI 2 min transmission power:

0 kW

0 hp

Overall length:

8.1 m

26.568 ft

Rotor diameter:

6.84 m

22.4352 ft

Tail rotor diameter:

1.29 m

4.2312 ft

Fuselage length:

5.8 m

19.024 ft

Overall height:

2.22 m

7.2816 ft

Main rotor blades chord:

0 m

0 ft

Tail rotor blades chord:

0 m

0 ft

Mast tilt angle:

0 °

Noise at flyover, level:

0 dB EPNL

Noise at flyover, limit:

0 dB EPNL

Noise at takeoff, level:

0 dB EPNL

Noise at takeoff, limit:

0 dB EPNL

Noise at landing, level:

0 dB EPNL

Noise at landing, limit:

0 dB EPNL

Crew:

0

Max pax number:

0

Average price:

190000 $