Popis
- sběratelský model vrtulníka 1/72 - provedení: kovový model s plastovými částmi - model je v kvalitním provedení - součástí balení je stojánek
Mil Mi-28 Havoc
The Mil Mi-28 (NATO reporting name „Havoc“) is a Russian all-weather, day-night, military tandem, two-seat anti-armor attack helicopter. It is an attack helicopter with no intended secondary transport capability, better optimized than the Mil Mi-24 gunship for the role. It carries a single gun in an undernose barbette, plus external loads carried on pylons beneath stub wings.
Role | Attack helicopter |
---|---|
National origin | Soviet Union/Russia |
Manufacturer | Mil |
First flight | 10 November 1982 |
Introduction | 15 October 2009 (Mi-28N) |
Status | In service |
Primary users | Russian Air Force Algerian Air Force Iraqi Air Force |
Produced | 1982–present |
Number built | 126 |
Unit cost |
US$15–16 million (2002)
|
The Russian Army received the first Mi-28 prototypes for testing in 2004.It received the first serial production Mi-28N in 2006, which then joined two prototype helicopters for army trials. The aircraft entered service in 2006.It has entered service under the name of „Night Hunter“ (Russian: Ночной охотник).A squadron of Mi-28Ns from Torzhok took part in a joint army exercise in Belarus in June 2006.
Mi-28
Prototype version; first flight in 1982.
Mi-28A
Original production anti-tank helicopter.
Mi-28N/MMW Havoc.
All weather day-night version. Equipped with a top-mounted millimeter wave radar station, thermographic camera-TV, and a laser rangefinder. Powered by two Russian Klimov TV3-117VMA-SB3 engines (2,500 hp each), produced by the Ukrainian Motor-Sich and replaced by Russian-made VK-2500 engines as of 2016. Max takeoff weight: 11,500 kg, max payload: 2,350 kg.
General characteristics
- Crew: Two: 1 pilot (rear), 1 navigator/weapons operator (front)
- Length: 17.91 m (58 ft 9 in)
- Rotor diameter: 17.20 m (56 ft 5 in)
- Height: 3.82 m (12.5 ft (150 in))
- Disc area: 232.35 m² (2,501 ft²)
- Empty weight: 7,890 kg (17,400 lb)
- Loaded weight: 10,500 kg (23,150 lb)
- Max. takeoff weight: 11,700 kg (25,800 lb)
- Powerplant: 2 × Klimov TV3-117 turboshaft, 1,636 kW (2,194 shp) each