General characteristics
- Crew: 2-3: pilot, weapons system officer and technician (optional)
- Capacity: 8 troops or 4 stretchers
- Length: 17.5 m (57 ft 4 in)
- Rotor diameter: 17.3 m (56 ft 7 in)
- Wingspan: 6.5 m (21 ft 3 in)
- Height: 6.5 m (21 ft 3 in)
- Disc area: 235 m² (2,530 ft²)
- Empty weight: 8,500 kg (18,740 lb)
- Max takeoff weight: 12,000 kg (26,500 lb)
- Powerplant: 2× Isotov TV3-117 turbines, 1,600 kW (2,200 hp) each
Performance
- Maximum speed: 335 km/h (208 mph)
- Range: 450 km (280 miles)
- Service ceiling: 4,500 m (14,750 ft)
- Armament
- Internal guns
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- 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 on the Mi-24P. 750 rounds of ammunition.
- flexible twin-barrel GSh-23L on the Mi-24VP and Mi-24VM. 450 rounds of ammunition.
- PKT passenger compartment window mounted machine guns
- External stores
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- 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
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- Bombs within weight range (presumably ZAB, FAB, RBK, ODAB etc.), Up to 500 kg.
- MBD multiple ejector racks (presumably MBD-4 with 4xFAB-100)
- KGMU2V submunition/mine dispenser pods
- First-generation armament (standard production Mi-24D)
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- GUV-8700 gunpod (with a 12.7 mm Yak-B + 2x7.62 mm GShG-7.62 mm combination or one 30 mm AGS-17)
- UB-32 S-5 rocket launchers
- S-24 240 mm rocket
- 9M17 Phalanga (a pair on each wingtip pylon)
- Second-generation armament (Mi-24V, Mi-24P and most upgraded Mi-24D)
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- 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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