Vertipedia - Mil Mi-24P

Variant of the Mil Mi-24 with the NATO designation of 'Hind F'. The helicopter has a pod and boom configuration, has a passenger capacity of 8, and is fitted with a 30 mm fixed gun mount. The engines are fitted with deflectors and separators for dust intake prevention. Onboard equipment allows operation during daytime and twilight under Visual Flight Rules (VFR) weather conditions.

Overview

Data on design, manufacture and status

Design authority: MVZ Mil

Primary manufacturer: MVZ Mil

Parent type: Mil Mi-24

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: 2 in Tandem arrangement

Landing gear: Wheels (all 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

Overall Dimensions
Overall Height:	3.97 m	13.0 ft
Overall Length:	21.35 m	70.0 ft
Overall Width:	17.30 m	56.8 ft

Airframe Dimensions
Airframe Length:	17.51 m	57.4 ft
Airframe Width:	6.66 m	21.9 ft
Airframe Height:	3.97 m	13.0 ft

Landing Gear Dimensions
Landing Gear Base:	4.39 m	14.4 ft
Landing Gear Track:	3.03 m	9.9 ft

Cabin Dimensions
Cabin Internal Height:	1.20 m	3.9 ft
Cabin Internal Length:	2.50 m	8.2 ft
Cabin Internal Width:	1.45 m	4.8 ft

Cruise Speed: 280 km/h

Weights
Max Gross Weight (ground):	11,500 kg	25,353 lb
Max Gross Weight (airborne):
Max Take-off Weight:	11,500 kg	25,353 lb
Empty Weight:	8,500 kg	18,739 lb

Climb Performance
Max Rate of Climb:	13 m/s	2,461 fpm

Hover Performance
Hover Ceiling IGE:
Hover Ceiling OGE:	1,500 m	4,921 ft

Limitations
Max Level Flight Speed:	320 km/h	173 kts
Never Exceed Speed:
Service Ceiling:	4,500 m	14,764 ft

Range and Endurance
Max Range:	440 km	238 nm
Max Endurance:	4 hrs

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

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

Normal Ratings
Max continuous:
Take-off / rated:	1640 kW	2198 hp
Intermediate:	1618 kW	2169 hp
Maximum:

OEI Ratings
OEI contingency:	1765 kW	2366 hp
OEI continuous:
OEI 30-second:
OEI intermediate:	1618 kW	2169 hp

Main Rotor Characteristics
Diameter:	17.30 m	56.76 ft
RPM:
Direction of Rotation:	Clockwise
Hub Type:

Main Rotor Blade Characteristics
Blade Construction:	Aluminum alloy spar, honeycomb core
Blade Chord:	0.580 m	1.90 ft
Blade Tip Geometry:	Conventional
Blade Twist:
Number of Blades:	5

Main Rotor Derived Characteristics
Disc Area:	235.06 m²	2530.3 ft²
Disc Loading:	48.92 kg/m²	10.020 lb/ft²
Solidity:	0.1067

Main Rotor Blade Derived Characteristics
Blade area per blade:	5.02 m²	54.0 ft²
Tip Speed:

Tail Rotor Characteristics
Diameter:	3.91 m	12.83 ft
Configuration:	Tractor
Direction of Rotation:	Top blade aft
RPM:

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

Tail Rotor Derived Characteristics
Disc Area:	12.01 m²	129.2 ft²
Solidity:

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

References

References and sources used

Russia's Arms Catalog: Volume II (Air Force)

Military Parade Ltd.
1996 (page 172)
Book

Russian Helicopters, Ka-27

Russian Нelicopters, JSC
5 July 2017 (page 218)
Website

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Main Rotor Diameter:	17.30 m	56.76 ft
Max Gross Weight (ground):	11,500 kg	25,353 lb

Number of engines:	2 Turbines
Max Level Flight Speed:	320 km/h	173 kts
Max Range:	440 km	238 nm
Max Endurance:	4 hrs	4 hrs