- Jul 1, 2018
- 1,635
| Product Type | Vehicle Production |
| Country | Russia |
| Product Name | Mil Mi-24VM |
| Product Quantity | 40 |
| Unit Cost | 16,721,532.00 |
| On the Catalogue? | Yes |
| Private / Encrypted? | No |
| Completion Date | Tue, 13 Dec 2022 |
| Total Cost | 668,861,280.00 |
| Product Information | 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 only 19.79 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 Maximum speed: 335 km/h (208 mph, 181 kn) Range: 450 km (280 mi, 240 nmi) Service ceiling: 4,900 m (16,100 ft) flexible twin-barrel GSh-23L autocannon. 450 rounds of ammunition. PKB passenger compartment window mounted machine guns 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 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 pods 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 |
