| Picture |
|
| Manufacturer |
Mil
|
| Type |
Mi-24 / Hind
|
| Introduced |
1/1/1972
|
| In production? |
Yes
|
| Units produced |
5200
|
| Price US $ |
0.00
|
| Overall Length |
70 ft
|
| Length |
57.4 ft
|
| Height |
17.9 ft
|
| Width |
0 ft
|
| |
|
| |
|
| Description |
Twin turbine, Russian multi purpose attack helicopter. The model Mi-25 and Mi-35 are export versions of the Mi-24.
|
| Advertisement |
|
| Design features |
- Tandem cockpit with "double bubble" canopy
- Heavily armored body
- Overpressurized cockpit to protect in NBC conditions
- Retractable tricycle undercarriage
- Two mid-mounted stub wings provide up to one quarter of total lift at high speed
- Main rotor tilted 2.5° to the right to counteract dissymmetry of lift at high speed
- Titanium rotor blades
- All-metal semi-monocoque fuselage pod and boom structure
|
|
Twin turbine, Russian multi purpose attack helicopter. The model Mi-25 and Mi-35 are export versions of the Mi-24.
|
|
- Advertisement -
|
Design features:
- Tandem cockpit with "double bubble" canopy
- Heavily armored body
- Overpressurized cockpit to protect in NBC conditions
- Retractable tricycle undercarriage
- Two mid-mounted stub wings provide up to one quarter of total lift at high speed
- Main rotor tilted 2.5° to the right to counteract dissymmetry of lift at high speed
- Titanium rotor blades
- All-metal semi-monocoque fuselage pod and boom structure
|
| Persons |
10
|
| Max. Range |
311 mi
|
| Cruise Speed |
168 mph
|
| Max. Speed |
208 mph
|
| Max. rate of Climb |
2460 ft/min
|
| HOGE ceiling |
4920 ft
|
| Service Ceiling |
14764 ft
|
| Gross Weight |
25353 lb
|
| Empty Weigt |
18387 lb
|
| Useful Load |
6966 lb
|
| Fuel Capacity |
563 gallons
|
| Number of Engines |
2
|
| Engine Type |
Turbine
|
| Engine Code |
Klimov TV3-117VM
|
| Horse Power |
2194
|
| Rotorhead |
Fully articulated
|
| Number of rotorblades |
5
|
| Rotor Diameter |
56.8 ft
|
| Number of tail rotorblades |
3
|
| Tailrotor Diameter |
12.8 ft
|
|