Vertipedia - Mil Mi-8PS

Mi-8 version for Head of State and VIP transport

Overview

Data on design, manufacture and status

Design authority: MVZ Mil

Primary manufacturer: MVZ Mil

Parent type: Mil Mi-8/Mi-14/Mi-17

Aircraft status: Status unknown

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift devices: 1 Single main rotor

Dedicated control device: 1 Tail rotor

Crew required: 3 in Other arrangement

Landing gear: Wheels (non-retractable)

Key Characteristics

Data on key physical features

Aircraft Details

Data on aircraft configuration, weights, flight performance and equipment

Layout and Dimensions

Weights and Performance

Engine Details

Primary Lift Device

Primary Control Device

Measurements do not specify Turning Rotors.

Overall Dimensions
Overall Height:	5.65 m	18.5 ft
Overall Length:	25.24 m	82.8 ft
Overall Width:	21.29 m	69.8 ft

Airframe Dimensions
Airframe Length:
Airframe Width:	2.50 m	8.2 ft
Airframe Height:

Landing Gear Dimensions
Landing Gear Base:	4.26 m	14.0 ft
Landing Gear Track:	4.80 m	15.7 ft

Cabin Dimensions
Cabin Internal Height:	1.80 m	5.9 ft
Cabin Internal Length:	6.36 m	20.9 ft
Cabin Internal Width:	2.34 m	7.7 ft

Max Speed: 250 km/h; Cruise Speed: 225 km/h

Weights
Max Gross Weight (ground):	13,000 kg	28,660 lb
Max Gross Weight (airborne):
Max Take-off Weight:	13,000 kg	28,660 lb
Empty Weight:

Climb Performance
Max Rate of Climb:

Hover Performance
Hover Ceiling IGE:
Hover Ceiling OGE:

Limitations
Max Level Flight Speed:
Never Exceed Speed:
Service Ceiling:	4,900 m	16,076 ft

Range and Endurance
Max Range:
Max Endurance:

Provided powerplant data is for uninstalled, sea level, static operations.

Powerplant
Number of engines:	2
Designation:	Motor Sich TV3-117 turbine
Manufacturer:	Motor Sich

Normal Ratings
Max continuous:
Take-off / rated:	1640 kW	2198 hp
Intermediate:
Maximum:

OEI Ratings
OEI contingency:
OEI continuous:
OEI 30-second:
OEI intermediate:

Main Rotor Characteristics
Diameter:	21.29 m	69.85 ft
RPM:
Direction of Rotation:	Clockwise
Hub Type:

Main Rotor Blade Characteristics
Blade Construction:
Blade Chord:
Blade Tip Geometry:	Conventional
Blade Twist:
Number of Blades:	5

Main Rotor Derived Characteristics
Disc Area:	355.99 m²	3832.0 ft²
Disc Loading:	36.52 kg/m²	7.479 lb/ft²
Solidity:

Main Rotor Blade Derived Characteristics
Blade area per blade:
Tip Speed:

Tail Rotor Characteristics
Diameter:
Configuration:	Pusher
Direction of Rotation:	Top blade fwd
RPM:

Tail Rotor Blade Characteristics
Number of Blades:	3
Blade Construction:
Blade Chord:
Blade Twist:

Tail Rotor Derived Characteristics
Disc Area:
Solidity:

Tail Rotor Blade Derived Characteristics
Tip Speed:
Blade Area (per blade):

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Resources related to the Mi-8PS , provided by public sources across the internet.

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Images

Overview

Attribution

Main rotor

Attribution

Tail rotor

Attribution

Miscellaneous

Attribution

Number of engines:	2 Turbines
Max Level Flight Speed:
Max Range:
Max Endurance:

Main Rotor Diameter:	21.29 m	69.85 ft
Max Gross Weight (ground):	13,000 kg	28,660 lb