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Mi24 - Helicopter

One of these is available, but I must stress some minor parts are missing, but everything is there to either start a restoration, or put on your front drive way. Only 200 Mi-24A helicopters were manufactured during the five years of their production. The operation of these helicopters, including combat missions, contributed greatly to their further development, updating and improved reliability. This also allowed training pilots and maintenance personnel both in our country and abroad.
     The operational experience of the Mi-24A revealed in particular the poor external view from the pilot's cockpit. This drawback forced a radical change in the helicopter nose to accommodate the new weapon systems and sights. In the final version, the pilot and weapon operator were seated in tandem, stepped cockpits under individual canopies. The unfixed mount with the YaKB-12.7 (Yakushev-Borzov) machine gun, boasted a high rate of fire (4,000-4,500 r.p.m) and was remotely controlled via the KPS-53AV sighting station and housed in the exterior front part of the weapon operator's cockpit. The cartridge box previously housed in the pilot's cockpit was installed under the cockpit floor and handled from the outside. There was another problem to solve: it involved the provision of a broad view (±60 deg. in azimuth) for the Raduga observation device used by the weapon operator, which would not impair visibility by structural members and similar view for the command radio link antenna. They were installed on both sides of the fuselage, below the outline of the machine-gun mount. This marked the final general appearance of the crew cockpit and of Mi-24D and Mi-24V as a whole. These helicopters jointly underwent state trials and were launched into series production.
     As mentioned earlier, the D version differed from the A version owing to the Phalanga-P antitank missile system incorporating Raduga-F semiautomatic guiding system, which increased the accuracy of antitank missiles two times. In addition, the gyrostabilizing guidance device provided for helicopter's maneuverability within ±60 degrees in yaw during missile guidance, thereby increasing its effectiveness. The provision of a remotely controlled machine gun USPU-24 for the equipment of the Mi-24D ensured automatic introduction of the corrections into firing. The system also comprised an analogue computer compatible with the airborne system of modulating transducers. The unguided armament of the Mi-24D helicopter was not changed, as was the case with the Mi-24A helicopter.
     Adoption of the final version of the helicopter Mi-24V was delayed by the development of a new generation Shturm-V antitank missile system. It should be noted here that the Shturm-V system was reviewed as a helicopter version of the ground system Shturm-S. However, the helicopter version was the first to become operational. In addition to the Shturm-V system, the ASP-17V, an automatic pilot's sight was mounted on the Mi-24V. This sight was a modification of the sight developed for the Su-17 aircraft.
     Consequently, the main work on the army transport-combat helicopter came to an end and the Mi-24D and Mi-24V became operational in conformity with Government Decree dated March 1976.
     The Mi-24 helicopter remained for a long time the powerful and effective combat vehicle. As a reward of their efforts, the main developers, including Designer General M.N.Tischenko, were awarded Lenin prizes. Meanwhile a large group of designers, workers and customer's representatives were given government awards. However, work on the Mi-24 was still not over. A roomy compartment to accommodate troops predetermined further development of utility versions, including: ? Mi-24P helicopter intended for chemical and radiation reconnaissance. This helicopter underwent a baptism of fire when determining the scope of the disaster at the Chernobyl nuclear power station; ? Mi-24K reconnaissance artillery spotting helicopter intended for ground forces.
     However, most development work on the Mi-24 was geared to increase its combat and fire power.

Please click here to view ACTUAL Mi24

Specifications

 Model: Mi24

 Length: 21.5m
 Height: 5.47
 Main rotor: 17.3m
 Number of rotor blades: 5
 Tail rotor blades: 3
 Engines: 2 x TV-3-117VM
 Model: Shaft horse power 2,200
 Weight empty: 8,620 kgs
 Weight max: 11,500 kgs
 Weight slung: 2,500 Kgs
 Max speed: 310 - 330 Km/h
 Range: 450 Kms
 Ceiling height: 2,200 m