Mi-35 dan Mi-17 Helicopter Specifications - Most Video Review

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 more than 30 other nations. In NATO circles, the export versions, Mi-25 and Mi-35, are denoted with a letter suffix as "Hind D" and "Hind E". Soviet pilots called the Mi-24 the "flying tank" (летающий танк; letayushchiy tank), a term used historically with the famous World War II Soviet Il-2 Shturmovik armored ground attack aircraft. More common unofficial nicknames were "Crocodile" (Крокодил; Krokodil), due to the helicopter's camouflage scheme and "Drinking Glass", (Стакан; Stakan) because of the flat glass plates that surround the Mi-24's cockpit.[2] Mi-24/Mi-25/Mi-35 Russian Mi-24PN Role Attack helicopter with transportcapabilities National origin Soviet Union/Russia Manufacturer Mil First flight 19 September 1969 Introduction 1972 Status In service Primary users Russian Air Force ca. 50 other users (see Operators section below) Produced 1969–present Number built 2,300 (estimated) Developed from Mil Mi-8 General characteristics Crew: 2–3: pilot, weapons system officer and technician (optional) Capacity: 8 troops or 4 stretchers or 2400 kg (5,291 lb) cargo on an external sling 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: 4,900 m (16076 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 on the Mi-24P. 750 rounds of ammunition. flexible twin-barrel Gryazev-Shipunov GSh-23L on the Mi-24VP and Mi-24VM. 450 rounds of ammunition. PKB passenger compartment window mounted machine guns External 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 pods First-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-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 ================================================= Mi-17 The Mil Mi-17 (NATO reporting name "Hip") is a Russian helicopter in production at two factories in Kazan andUlan-Ude. It is known as the Mi-8M series in Russian service. It is a medium twin-turbine transport helicopter. There are also armed gunship versions. Mi-17 / Mi-8M A Mi-17 from the Afghan Air Force takes off from Kabul International Airport Role Transport helicopter National origin Soviet Union Design group Mil Moscow Helicopter Plant Built by Kazan Helicopter Plant First flight 1975 Introduction 1977 (Mi-8MT), 1981 (Mi-17) Status In service Primary users Russia ca. 60 other countries Produced 1977–present Number built about 12,000[1] Unit cost Prices vary based on specifications (military and civilian prices differ) Developed from Mil Mi-8 General characteristics Crew: Three – two pilots and one engineer Capacity: 30 troops or 12 stretchers or 4,000 kg (8,820 lb) cargo internally /5,000 kg (11,023 lb) externally slung. Length: 18.465 m (60 ft 7 in) Rotor diameter: 21.25 m (69 ft 10½ in) Height: 4.76 m (15 ft 7¼ in) Disc area: 356 m² (3,834 ft²) Empty weight: 7,489 kg (16,510 lb) Loaded weight: 11,100 kg (24,470 lb) Max. takeoff weight: 13,000 kg (28,660 lb) Powerplant: 2 × Klimov TV3-117VM turboshafts, 1,633 kW (2,190 shp) each Performance Maximum speed: 250 km/h (135 knots, 155 mph) Range: 465 km (251 nmi, 289 mi) (standard fuel) Service ceiling: 6,000 m (19,690 ft) Rate of climb: 8 m/s[citation needed] (1,575 ft/min) Armament up to 1,500 kg (3,300 lb) of disposable stores on six hardpoints, including bombs, rockets, and gunpods. wikipedia.org

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