Russian Mil Mi-24

Used by US Army in "Aggressor" Training

The Mil Mi-24 (Миль Ми-24, NATO reporting name: Hind) is a large helicopter gunship and attack helicopter and low-capacity troop transport with room for eight passengers. It is produced by Mil Moscow Helicopter Plant and operated since 1972 by the Soviet Air Force, its successors, and 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" respectively. Soviet pilots called the Mi-24 the "flying tank", or летающий танк (letayushchiy tank). More common unofficial nicknames were "Crocodile" (Крокодил or Krokodil) due to the helicopter's camouflage scheme and "Drinking Glass" (Стакан or Stakan) because of the flat glass plates which surround the cockpit of the Mi-24.

Role Attack helicopter with transport capabilities
National origin Soviet Union
Manufacturer Mil
First flight 19 September 1969
Introduction 1972
Status In service
Primary users Russian Air Force
ca. 50 other users
Produced 1969–present
Number built 2,300 (estimated)
Developed from Mil Mi-8

Design

Overview

Russian Air Force Mi-35М

The core of the aircraft was derived from the Mil Mi-8 (NATO reporting name "Hip"): two top-mounted turboshaft engines driving a mid-mounted 17.3 m five-blade main rotor and a three-blade tail rotor. The engine configuration gave the aircraft its distinctive double air intake. Original versions have an angular greenhouse-style cockpit; Model D and later have a characteristic tandem cockpit with a "double bubble" canopy. Other airframe components came from the Mi-14 "Haze". Two mid-mounted stub wings provide weapon hardpoints, each offering three stations, in addition to providing lift. The load-out mix is mission dependent; Mi-24s can be tasked with close air support, anti-tank operations, or aerial combat.

The body is heavily armored and can resist impacts from .50 caliber (12.7 mm) rounds from all angles, including the titanium rotor blades. The cockpit is protected by ballistic-resistant windscreens and a titanium-armored tub. The cockpit and crew compartment are over-pressurized to protect the crew in NBC conditions.

Flight characteristics

Mi-24D cockpit

Considerable attention was given to making the Mi-24 fast. The airframe was streamlined, and fitted with retractable tricycle undercarriage landing gear to reduce drag. The wings provide considerable lift at high speed, up to a quarter of total lift. The main rotor was tilted 2.5° to the right from the fuselage to compensate for translating tendency at a hover. The landing gear was also tilted to the left so the rotor would still be level when the aircraft was on the ground, making the rest of the airframe tilt to the left. The tail was also asymmetrical to give a side force at speed, thus unloading the tail rotor.

A modified Mi-24B, named A-10, was used in several speed and time-to-climb world record attempts. The helicopter had been modified to reduce weight as much as possible, and among the measures used was to remove the stub wings. The speed record over a closed 1000 km course set on 13 August 1975 of 332.65 km/h still stands, as do many of the female specific records set by the all female crew of Galina Rastorgoueva and Ludmila Polyanskaia. On 21 September 1978 the A-10 set the absolute speed record for helicopters with 368.4 km/h over a 15/25 km course. The record stood until 1986 when it was broken by the current record holder, a modified Westland Lynx.

U.S. operated Mi-24P Hind-F

Comparison to Western helicopters

As a combination of armored gunship and troop transport, the Mi-24 has no direct NATO counterpart. While the UH-1 ("Huey") helicopters were used in the Vietnam War either to ferry troops, or as gunships, they were not able to do both at the same time. Converting a UH-1 into a gunship meant stripping the entire passenger area to accommodate extra fuel and ammunition, and removing its troop transport capability, while it has no armour. The Mi-24 was designed to do both, and this was greatly exploited by airborne units of the Soviet Army during the 1980–89 Soviet war in Afghanistan. The closest Western equivalent was the Sikorsky S-67 Blackhawk, which used many of the same design principles and was also built as a high-speed, high-agility attack helicopter with limited troop transport capability. It was also designed using many components from the existing Sikorsky S-61. The S-67, however, was never adopted for service. Another relatively close western equivalent, yet not armored, is the MH-60 Direct Action Penetrator, a special purpose variant of the Sikorsky UH-60 Black Hawk, which is capable of mounting a variety of weapons on its stub wings, including AGM-114 Hellfire missiles and Hydra 70 rockets.

Specifications (Mi-24)

Orthographic projection of the Mil Mi-24.
Cabin door to the rear troop-utility compartment
Possible armament configuration on Mi-24W
Yakushev-Borzov YakB-12.7 machine gun
Mi-35

Data from Indian-Military.org

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 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 Phalanga (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

Source

The information contained on this page is unclassified, approved for public dissemination and is released under CC-BY-SA Licensing Agreement.



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