Mil

Manufacturer:

Mil

Country:

Russia

Commercial designation:

Havoc

Technical designation:

Mi-28

Version, Variant:

A

Type:

Conventional

Currently produced:

N

Typical missions:

Military Combat Attack

Flight conditions:

VFR

First flight:

1987

Landing system:

wheels

Blades number:

5

Tail blades number:

3

MTOW with external loads:

11500 kg

25357.5 lbs

MTOW with only internal loading:

11500 kg

25357.5 lbs

Empty weight:

8095 kg

17849.475 lbs

External payload:

2300 kg

5071.5 lbs

Internal payload:

0 kg

0 lbs

Standard fuel tank:

1337 kg

2948.085 lbs

with optionnal external fuel tank:

1782 kg

3929.31 lbs

Cruise speed:

265 km/h

143.1 kt

Maximum cruise speed:

0 km/h

0 kt

Vne:

300 km/h

162 kt

Max negative g @ MTOW:

-0.5 g

Max positive g @ MTOW:

3 g

Range with normal tanks:

460 km

248.4 nm

Max range with auxiliary external tanks:

1100 km

594 nm

Max endurance @ min consumption speed:

02:00:00 h:min

Rate of climb @ SL:

13.6 m/s

2676.48 ft/min

Rate of climb @ SL @MTOW:

0 m/s

0 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:

3600 m

11808 ft

OGE max hovering altitude, empty:

0 m

0 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:

5800 m

19024 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:

Engine manufacturer:

Klimov

Model:

TV3-117VMA

Engines quantity:

2

Powerplant category:

turbine

Main rotor rotation speed:

242 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:

2900 kW

3941.1 hp

Transmission shaft max continuous power:

0 kW

0 hp

Transmission shaft max power:

0 kW

0 hp

Takeoff power 5 min:

0 kW

0 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:

0 m

0 ft

Rotor diameter:

17.2 m

56.416 ft

Tail rotor diameter:

3.85 m

12.628 ft

Fuselage length:

16.89 m

55.3992 ft

Overall height:

4.73 m

15.5144 ft

Main rotor blades chord:

0.67 m

2.1976 ft

Tail rotor blades chord:

0.24 m

0.7872 ft

Mast tilt angle:

5 °

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:

2

Max pax number:

3

Average price:

0 $