Design and development
The MiG-27 shares the basic airframe of the MiG-23, but with a revised nose — nicknamed "Utkonos" ("Platypus") in Russian service, first introduced on the MiG-23B. Dissatisfaction with the MiG-23BN led to the further development of the basic airframe to accommodate a stronger undercarriage, simpler intakes and a shorter exhaust nozzle, without radar in favor of a downward-sloping profile for improved pilot visibility,[clarification needed] a laser rangefinder and marked-target seeker. Among its test pilots, it was also called "Balkon" ("Balcony") because of the increased frontal view from the cockpit. Additional cockpit armor was installed, along with a totally new nav/attack system.Since the MiG-27 was intended to fly most of its missions at low altitude, the MiG-23's variable intake ramps and exhaust nozzles were discarded in favor of a simpler fixed configuration, reducing weight and maintenance requirements. The aircraft also has larger, heavy-duty landing gear to facilitate operation from poorer-quality airfields. With the for strike and low-level attack requirements, provisions were made to mount missiles and precision-guided munitions, as well as retaining a nuclear capability in line with other Soviet combat aircraft by introducing specialized navigation systems.
Operational history
It was used by Soviet forces during the later stages of the Afghanistan conflict in 1987–1989.Although Western military analysts considered the MiG-27 widely exported, the aircraft type was primarily used by Soviet client states and India. Other operators utilized the MiG-27 in a variety of regional conflicts.
Sri Lanka
MiG-27 aircraft entered service with the Sri Lanka Air Force in 2000. During the Sri Lankan Civil War, they saw considerable action bombing strategic targets and providing close air support. In August 2000, a MiG-27 crashed near Colombo International Airport, killing its Ukrainian pilot. In July 2001, a second MiG-27 was destroyed on the ground during an assault on the same air force base by the Liberation Tigers of Tamil Eelam. MiG-27 crashed into the sea near the airport in June 2004. Another MiG 27 fighter jet crashed on a routine training mission in 13th Feb. 2012 near Dummalasuriya area at around 1.35 p.m. The pilot managed to eject the jet without sustaining injuries.India
On 27 May 1999, during the Kargil War, one Indian MiG-27 was lost together with a MiG-21 while supporting an Indian ground offensive in the Kashmir region.Since 2001, the Indian Air Force has lost 12 MiG-27s to crashes. In mid-February 2010, India grounded its entire fleet of over 150 of the aircraft after a MiG-27 crashed on 16 February 2010 in Siliguri, West Bengal. The crash was attributed to defects in the R 29 engines of the aircraft, suspected to have occurred during the overhauling of the aircraft by Hindustan Aeronautics Limited [HAL].
Kazakhstan
The MiG-27 remains in service with the Kazakh Air Force.Variants
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- MiG-23B
- MiG-23BN
- MiG-27 (MiG-23BM)
- MiG-27K
- MiG-27M
- MiG-27D
- MiG-27ML
- MiG-27H
Operators
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Current operators
- Indian Air Force : 145 in service
- Sri Lanka Air Force : 7 in service
- Kazakh Air and Air Defence Forces : An estimated 40 MiG-23UB/MiG-27 are still operational.
Former operators
- The Cuban Air Force received 15 MiG-27s.
- The Iranian Air Force acquired a number of MiG-27 from the Soviet Union. They appear to be inactive.
- The Russian Air Force retired their aircraft from front-line use. They are still in reserve and in storage.
- The Ukrainian Air Force has retired their aircraft.
- The Soviet Air Force passed their aircraft on to successor states.
Specifications (MiG-27K)
Data from[citation needed]
General characteristics- Crew: 1 Pilot only
- Length: 17.08 m (56 ft 0 in) ()
- Wingspan:
- Height: 5 m (16 ft 5 in) ()
- Wing area:
- Empty weight: 11,908 kg (26,253 lb) (equipped) ()
- Loaded weight: 20,300 kg (44,800 lb) ()
- Max. takeoff weight: 20,670 kg (45,570 lb) ()
- Powerplant: 1 × Khatchaturov R-29B-300 afterburning turbojet
- Dry thrust: 78.5 kN (17,650 lbf) ()
- Thrust with afterburner: 112.8 kN (25,360 lbf) ()
- Maximum speed:
- Combat radius: 780 km (480 mi) ()
- Ferry range: 2,500 km (1,550 mi) ()
- Service ceiling: 14,000 m (46,000 ft) ()
- Rate of climb: 200 m/s (39,400 ft/min) ()
- Wing loading: 605 kg/m² (123.9 lb/sq ft) ()
- Thrust/weight: 0.62
- Guns:
- Hardpoints: One centerline, four fuselage, and two wing glove pylons with a capacity of 4,000 kg (8,800 lb)
- Missiles: pre-installed rocket pods for various (optional) laser, TV and electro-optically guided ASMs and PGMs
- Bombs: general-purpose bombs (optional)
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