Unit cost: 12,000,000–12,000,000 USD
Length: 17.5 m
Wingspan: 6.5 m
Height: 6.5 m
Max takeoff weight: 12,000 kg
Engine: 2 × TV3-117
Maximum speed: 335 km/h
Range: 450 km
Service ceiling: 4900 m
Capacity: up to 8 troops
Total ammunition payload: up to 1500 kg
Armament: Variety of bombs, missiles and rockets
Origin: Soviet Union (Russia)
Length: 17.5 m
Wingspan: 6.5 m
Height: 6.5 m
Max takeoff weight: 12,000 kg
Engine: 2 × TV3-117
Maximum speed: 335 km/h
Range: 450 km
Service ceiling: 4900 m
Capacity: up to 8 troops
Total ammunition payload: up to 1500 kg
Armament: Variety of bombs, missiles and rockets
Origin: Soviet Union (Russia)
The Mil Mi-24 (Russian: Миль Ми-24; NATO reporting name: Hind) is a large helicopter gunship, attack helicopter and low-capacity troop transport with room for eight passengers.[1] It is produced by Mil Moscow Helicopter Plant and has been operated since 1972 by the Soviet Air Force and its successors, along with 48 other nations.
General characteristics
- Crew: 2-3 pilot, weapons system officer and technician (optional)
- Capacity: 8 troops / 4 stretchers / 2,400 kg (5,291 lb) cargo on an external sling
- Length: 17.5 m (57 ft 5 in) fuselage only19.79 m (65 ft) including rotors
- Wingspan: 6.5 m (21 ft 4 in) stub wings
- Height: 6.5 m (21 ft 4 in)
- Empty weight: 8,500 kg (18,739 lb)
- Max takeoff weight: 12,000 kg (26,455 lb)
- Powerplant: 2 × Isotov TV3-117 turboshaft engines, 1,600 kW (2,200 shp) each
- Main rotor diameter: 17.3 m (56 ft 9 in)
- Main rotor area: 235.1 m2 (2,531 sq ft) NACA 23012[137]
Performance
- Maximum speed: 335 km/h (208 mph, 181 kn)
- Range: 450 km (280 mi, 240 nmi)
- Service ceiling: 4,900 m (16,100 ft)
Armament
Internal guns
- flexible 12.7 mm Yakushev-Borzov Yak-B Gatling gun on most variants. Maximum of 1,470 rounds of ammunition.
- fixed twin-barrel GSh-30K autocannon on the Mi-24P. 250 rounds of ammunition.
- flexible twin-barrel GSh-23L autocannon on the Mi-24VP and Mi-24VM. 450 rounds of ammunition.
- flexible GIAT dual feed 20mm (M693) autocannon on Mi-24 SuperHind Mk.II/III/IV/V. 320 rounds of ammunition.
- PKB passenger compartment window mounted machine gunsExternal stores
- Total payload is 1,500 kg of external stores.
- Inner hardpoints can carry at least 500 kg
- Outer hardpoints can carry up to 250 kg
- Wing-tip pylons can only carry the 9M17 Phalanga (in the Mi-24A-D) or the 9K114 Shturm complex (in the Mi-24V-F).Bomb-load
- Bombs within weight range (presumably ZAB, FAB, RBK, ODAB etc.), up to 500 kg.
- MBD multiple ejector racks (presumably MBD-4 with 4 × FAB-100)
- KGMU2V submunition/mine dispenser podsFirst-generation armament (standard production Mi-24D)
- GUV-8700 gunpod (with a 12.7 mm Yak-B + 2 × 7.62 mm GShG-7.62 mm combination or one 30 mm AGS-17)
- UB-16 S-5 rocket launchers
- UB-32 S-5 rocket launchers
- S-24 240 mm rocket
- 9M17 Fleyta (a pair on each wingtip pylon)Second-generation armament (Mi-24V, Mi-24P and most upgraded Mi-24D)
- UPK-23-250 gunpod carrying the GSh-23L
- B-8V20 a lightweight long tubed helicopter version of the S-8 rocket launcher
- 9K114 Shturm in pairs on the outer and wingtip pylons
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