Altaya – Mil Mi-28N Havoc,Russian Air Force

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                               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

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