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Sikorsky

S-80M MH-53 E

S-80 is the export version of MH-53E, only delivered to Japan

tags: Military Naval

aircraft

Manufacturer:

Sikorsky

Country:

USA

Commercial designation:

S-80M

Technical designation:

MH-53

Version, Variant:

E

Type:

Conventional

Currently produced:

N

Typical missions:

Military Naval

Flight conditions:

IFR

First flight:

0

Landing system:

wheels

Blades number:

6

Tail blades number:

4

weight

MTOW with external loads:

0 kg

0 lbs

MTOW with only internal loading:

0 kg

0 lbs

Empty weight:

0 kg

0 lbs

External payload:

16000 kg

35280 lbs

Internal payload:

16000 kg

35280 lbs

Standard fuel tank:

9930 kg

21895.65 lbs

with optionnal external fuel tank:

0 kg

0 lbs

performance

Cruise speed:

0 km/h

0 kt

Maximum cruise speed:

0 km/h

0 kt

Vne:

0 km/h

0 kt

Max negative g @ MTOW:

0 g

Max positive g @ MTOW:

0 g

Range with normal tanks:

0 km

0 nm

Max range with auxiliary external tanks:

0 km

0 nm

Max endurance @ min consumption speed:

00:00:00 h:min

Rate of climb @ SL:

0 m/s

0 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:

0 m

0 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:

0 m

0 ft

Max operating altitude, empty weight:

0 m

0 ft

Highest use Temperature:

0 °C

0 °F

Lowest use Temperature:

0 °C

0 °F

power

APU in HC:

Engine manufacturer:

General Electric

Model:

T64-GE-416

Engines quantity:

3

Powerplant category:

turbine

Main rotor rotation speed:

0 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:

3230 kW

4389.57 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

dimensions

Overall length:

30.19 m

99.0232 ft

Rotor diameter:

24.08 m

78.9824 ft

Tail rotor diameter:

6.1 m

20.008 ft

Fuselage length:

22.35 m

73.308 ft

Overall height:

8.97 m

29.4216 ft

Main rotor blades chord:

0.76 m

2.4928 ft

Tail rotor blades chord:

0 m

0 ft

Mast tilt angle:

0 °

noise

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 and pax

Crew:

6

Max pax number:

55

use

Average price:

0 $

front side

Sikorsky S-80M MH-53 E

African Lion 2012

Sikorsky S-80M MH-53 E

enormous rotor and tail

Sikorsky S-80M MH-53 E

rear side

Sikorsky S-80M MH-53 E

from above

Sikorsky S-80M MH-53 E