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Sukhoi Su-27 ASCC codename: Flanker Multi-Role Fighter |
DESCRIPTION:
Marking a major improvement in the quality of Soviet fighters, the Su-27 is a long-range air superiority fighter comparable to the US F-15 in size and mission. The Su-27 is equipped with an analog fly-by-wire control system, a powerful pulse-Doppler radar, and up to ten air-to-air missiles giving it a potent look-down shoot-down capability. The Flanker also features a rearward-facing radar at the end of a long boom placed between the engines allowing the Su-27 to search for targets behind the aircraft. The Su-27's high thrust-to-weight ratio and refined aerodynamics allow superb flight characteristics at high angles of attack. In addition, the Soviet Navy purchased an improved Su-27K design, later redesignated the Su-33, to operate off its first class of large aircraft carriers. The Su-33 features canards for improved maneuverabilty as well as a strengthened airframe for carrier operations. An interesting feature of the Su-27 is its autopilot which is able to return the aircraft to right-side-up level flight at any altitude when the pilot presses a "panic-button." Besides the Su-33, the basic Su-27 airframe has also been developed into the Su-30, Su-35 and Su-37 fighters as well as the Su-34 bomber.
Data below for Su-27S 'Flanker-B' and Su-27UB 'Flanker-C' |
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HISTORY: | |
First Flight |
(T10-1) 20 May 1977 (T10-3) 23 August 1979 (T-10S-1) 20 April 1981 (Su-27UB) 7 March 1985 |
Service Entry
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December 1984
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CREW: |
one: pilot
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ESTIMATED COST:
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$40 to $70 million
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AIRFOIL SECTIONS: | |
Wing Root | unknown (5%) |
Wing Tip
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unknown (5%)
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DIMENSIONS: | |
Length | 71.92 ft (21.94 m) |
Wingspan | 48.17 ft (14.70 m) |
Height |
(Su-27S) 19.42 ft (5.92 m) (Su-27UB) 20.83 ft (6.36 m) |
Wing Area | 667.8 ft² (62.04 m²) |
Canard Area
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not applicable
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WEIGHTS: | |
Empty |
(Su-27S) 36,115 lb (16,380 kg) (Su-27UB) 38,580 lb (17,500 kg) |
Normal Takeoff |
(Su-27S) 51,015 lb (23,140 kg) (Su-27UB) 53,220 lb (24,140 kg) |
Max Takeoff |
(Su-27S) 62,390 lb (28,300 kg) (Su-27S) 72,750 lb (33,000 kg) [final production lot] (Su-27UB) 67,130 lb (30,450 kg) |
Fuel Capacity |
internal: 20,725 lb (9,400 kg) external: none |
Max Payload
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8,820 lb (4,000 kg) normal load 17,640 lb (8,000 kg) maximum allowable load |
PROPULSION: | |
Powerplant | two Saturn/ Lyul'ka AL-31F afterburning turbofans |
Thrust |
33,510 lb (149.06 kN) 55,116 lb (245.18 kN) with afterburner |
PERFORMANCE: | |
Max Level Speed |
at altitude: (Su-27S) 1,555 mph (2,500 km/h) at 36,090 ft (11,000 m), Mach 2.35 (Su-27UB) 1,335 mph (2,150 km/h) at 36,090 ft (11,000 m), Mach 2.0 at sea level: 870 mph (1,400 km/h), Mach 1.14 |
Initial Climb Rate | unknown |
Service Ceiling |
(Su-27S) 60,700 ft (19,000 m) (Su-27UB) 57,400 ft (17,500 m) |
Range |
typical: 1,510 nm (2,800 km) ferry: (Su-27S) 2,010 nm (3,720 km) (Su-27UB) 1,620 nm (3,000 km) |
g-Limits |
+9
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ARMAMENT: | |
Gun | one 30-mm GSh-301 cannon (150 rds) |
Stations | ten external hardpoints: two tandem under the fuselage centerline, two under the air ducts, four under the wings, two on the wingtips |
Air-to-Air Missile | R-60/AA-8 Aphid, up to six R-27R/T AA-10 Alamo-A/B, up to four R-27ER/ET AA-10 Alamo-C/D, R-73/AA-11 Archer, R-33/AA-9 Amos |
Air-to-Surface Missile | none |
Bomb | free-fall, cluster bombs |
Other |
rocket pods, ECM pods
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KNOWN VARIANTS: | |
T-10 'Flanker-A' | Original prototype, suffered from excessive drag, weak structure, excessive weight, and flutter; four built |
T-10S | Redesigned prototype |
P-42 | Third Su-27S prototype (T10S-3) modified to set several climb and altitude records |
T10-20R | Special conversion testbed used for long-range supersonic flight |
Su-27 'Flanker-A' | Production model prototype and development aircraft; 15 built |
Su-27S 'Flanker-B' | First production model with refined aerodynamics and an aft radar extension, single-seat model designed for dual-role air defense and ground attack missions |
Su-27SK | Export version of the Su-27S |
Su-27SKM | Updated variant of the Su-27S for export |
Su-27SM | Upgrade program for the Su-27S |
Su-27P 'Flanker-B' | Identical to the Su-27S but designed purely as an air defense interceptor and equipped with an in-flight refueling probe |
Su-27UB 'Flanker-C' | Two-seat combat-capable trainer with an improved radar in a longer nose |
Su-27PU 'Flanker-C' | Prototype of the Su-30 fighter bomber |
Su-27K 'Flanker-D' | Prototype of the Su-33 navalized fighter, also referred to as the T-10K |
Su-27KU or Su-27IB | Prototype of the Su-34 bomber |
Su-27M 'Flanker-E' | Prototype of the Su-35 fighter |
J-11 | Chinese designation for the Su-27, perhaps up to 300 to be license built in China |
J-11B |
Improved version of the Su-27SK developed by China that features major upgrades including a new radar and
an infrared search and track system while also incorporating Chinese weapons, reports suggest further
orders for the Su-27SK (J-11) built in Russia are to be cancelled in favor of constructing the J-11B
locally in China
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KNOWN COMBAT RECORD: |
Abkhaz-Georgian Civil War (Abkhazia, Russia, 1992-1994) Eritrean-Ethiopian War (Ethiopia, 1998-2000) Angola civil war (2000-2002) South Ossetia War (Russia, 2008) |
KNOWN OPERATORS: |
Abkhazia (Abkhazian Air Force) Angola, Força Aérea Popular de Angola (Angolan People's Air Force) Belarus, Voyenno Vozdushnyye Sily (Belarus Air Force) China, Zhongkuo Shenmin Taifang Tsunputai (People's Liberation Army Air Force) Eritrea (Eritrean Republic Air Force) Ethiopia, Ye Ityopya Ayer Hayl (Ethiopian Air Force) Indonesia, Tentara Nasional Indonesia - Angkatan Udara (Indonesian Air Force) Kazakhstan (Kazakhstan Air Force) Russia, Voyenno Vozdushniye Sili (Russian Air Force) Russia, Aviatsiya Voyenno-Morskoyo Flota Sily Rossii (Russian Naval Aviation) Ukraine, Voyenno Vozdushnyye Sily (Ukraine Military Air Forces) Union of Soviet Socialist Republics, Voyenno Vozdushniye Sili (Soviet Air Force) Uzbekistan (Uzbek Air Force) Vietnam, Khong Quan Nhan Dan Viet Nam (Vietnam People's Army Air Force) United States (US Air Force) |
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