https://en.wikipedia.org/wiki/Mil_Mi-28
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.
The Mi-28 is a new-generation attack helicopter that functions as an air-to-air
and air-to-ground partner for the Mi-24 Hind and Ka-50 Hokum. The five-blade
main rotor is mounted above the body midsection, and short, wide, tapered,
weapon-carrying wings are mounted to the rear of body midsection. Two turboshaft
engines in pods are mounted alongside the top of the fuselage with downturned
exhausts. The fuselage is slender and tapers to the tail boom and nose. It
features a tandem, stepped-up cockpits and a cannon mounted beneath the belly,
with non-retractable tricycle tail-wheel type landing gear. This
energy-absorbing landing gear and seats protect the crew in a crash landing or
in a low-altitude vertical fall. The crew is able to survive a vertical fall of
up to 12 m/s. The Mi-28 has a fully armoured cabin, including the windshield,
which withstands impact by 7.62 and 12.7mm armor piercing bullets and 20mm shell
fragments.
It is equipped with two heavily armored cockpits, a windshield able to withstand
rotor (55 deg), with reduced noise characteristics. It is powered by two 2,200
hp Isotov TV-3-117VM (t/n 014) turboshaft engines.
While the Mi-28 is not intended for use as a transport, it does have a small
passenger compartment capable of carrying three people. The planned purpose of
this is to enable the rescue of downed helicopter crews.
The Night attack variant helicopter retains most of the structural design of the
original Mi-28. The main difference is the installation of an integrated
electronic combat system. Other modifications include: new main gearbox for
transmitting higher power to the rotor; new high-efficiency blades with
swept-shaped tips; and an engine fuel injection control.
The pilot uses a helmet-mounted target designator, which allocates the target to
the navigator's surveillance and fire control system. The navigator/weapons
officer is then able to deploy guided weapons or guns against the target. The
targeting system follows the direction of the pilot's eyes.
The Mi-28 is equipped with a chin-mounted 30 mm Shipunov 2A42 autocannon. The
cannon is select fire, and has a dual-feed, which allows for a cyclic rate of
fire between 200 rounds per minute to 550 rounds per minute. Its effective range
varies from 1,500 meters for ground vehicles to 2,500 meters for air targets.
Rounds from High Explosive Incendiary (HEI) to Armour-Piercing Discarding Sabot
(APDS) can be used. Stated penetration for the 3UBR8 is 25 mm of RHA at 1,500
meters.
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
Number built
126
Unit cost
The Russian Air Force had 24 Mi-28s in service in February 2011.
The Russian Defense Ministry will procure up to 60 Mi-28UB training versions by
2020. The version will speed up and improve pilot training. Four to six Mi-28UBs
will be purchased for every unit that operates the Mi-28N. In 2013, it was
reported that the Mi-28N was to replace the Mil Mi-24 in the Russian Armed
Forces by 2015; however, the Russian Air Force still operates a large number of
Mi-24 and Mi-35 helicopters as of 2016, including some being deployed for combat
in Syria.
During the Battle of Palmyra in 2016, Russian Aerospace forces' Mil Mi-28
supported the Syrian Arab Army in their advance towards the city.
Specifications (Mi-28N)
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))
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)
Performance
Maximum speed: 324 km/h (175 knots, 201 mph)
Cruise speed: 265 km/h (145 knots, 164 mph)
Range: 435 km (234 nmi, 270 mi)
Combat radius: 200 km (108 nmi, 124 mi) ; with 10 min loiter and 5% reserves
Ferry range: 1,105 km (595 nmi, 685 mi)
Service ceiling: 4,950 m (16,250 ft)
Rate of climb: 13.6 m/s (816 m/min, 2,677 ft/min)
Power/mass: 0.31 kw/kg for TV3-117 ()
Hovering ceiling: 3,600 m (11,811 ft)
Armament
horizontal fire)
Hardpoints: Two pylons under each stub wing to mount bombs, rockets, missiles,
and gun pods. Main armament configurations include: 16 Ataka-V anti-tank
missiles and 40 S-8 rockets, Or
16 Ataka-V anti-tank missiles, and 10 S-13 rocket, Or
16 Ataka-V anti-tank missiles, and two 23 mm UPK-23-250 gun pods each containing
a GSh-23L with 250 rounds.
Other ordnance: 9K118 Sheksna, 9A-2200, and 9M123 Khrizantema anti-tank
missiles, 8 Igla-V and Vympel R-73 air-to-air missiles, 2 KMGU-2 mine dispensers
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