Military Factory
flag of Soviet Union

Sukhoi Su-17 / Su-20 / Su-22 (Fitter) Ground Attack / Strike Fighter (1970)

Authored By Captain Jack | Last Updated: 9/14/2013

The Su-17 Fitter - and its export derivatives, the Su-20 and Su-22 - were swing-wing developments of the original Su-7 Fitter fixed-wing design.

The Mach 2-capable Sukhoi Su-17 "Fitter" was a further development of the successful Su-7 "Fitter-A" fighter/fighter-bomber family line detailed elsewhere on this site. The aircraft incorporated a partial variable geometry wing ("swing wing") system and improved upon the former's take-off and landing attributes as well as performance at the low-level as required of it during ground attack runs. The swing-wing element added to the aircraft's stability at low-speeds and altitudes while improving overall range and ordnance loads by featuring large-area fixed wing "gloves". Beyond its new wing arrangement, the Su-17 also differed from its Su-7 origins in that it featured a newly-designed canopy and nose assembly as well as an identifiable raised fuselage spine, giving the new aircraft a more stout appearance than the pencil-thin Fitter-A. The type served the Soviet Union well and was heavily exported to Warsaw Pact nations and trusted Third World allies alike. The Su-17 was developed into the export Su-20 and Su-22 Fitter models of varying avionics, engines and weapons. In all, some 2,867 Su-17/Su-20/Su-22 Fitters were produced with almost half of these made available to Soviet export customers. Over a dozen nations took delivery of the type, making it a staple fighter-bomber throughout the Cold War. Some air forces continue to fly the aircraft - nearly forty years after it was introduced.

Development - Fitter-B

The Su-7 (NATO codename of "Fitter-A") was a capable aircraft in its own right. However, there were glaring deficiencies in its operational range - no thanks to a thirsty powerplant - and ordnance-carrying capabilities. Sukhoi and Soviet authorities sought other improvements that would make the Fitter series a much more capable and versatile battlefield component. As such, a Su-7BM production model served as the demonstrator for the testing of a new swing-wing variable geometry system development. The new wing would essentially be made up of two parts - a fixed wing root/wing glove and the positional swing-wing portion making up half of the wing (at about mid-wing span). The new prototype became the Su-7IG ("IG" for "Izmenyaemaya Geometriya", also internal designation of "S-22I"). First flight was achieved on August 2nd, 1966. The working prototype/technology demonstrator showed enough promise during this testing phase, improving on both field performance and range of the Su-7, that it was selected for production.

A two-seat Su-7U long-fuselage trainer was then revised. The rear instructor's cockpit would make way for additional avionics and fuel while housing the new wing component. The swing-wing configuration was devised as a way to increase the Su-7's inherent range while at the same time allowing the aircraft to carry more weaponry along its fixed wing portion without the need to implement heavy and complex swiveling weapon stations to maintain aerodynamic integrity in full sweep. A limited production run appeared under the base "Su-17" designation, these being fitted with the Lyulka AL-7F-1 turbojet powerplant of 22,046lbs thrust. Production of this early Fitter-B would run from 1969 to 1973.

The Su-17K became the export version of this base Su-17, though this was only received by the Egyptian Air Force. NATO assigned the new aircraft design the codename of "Fitter-B", sequentially relating this new design with that of the original Su-7 it originated from.

Text ©2003-2014 All Rights Reserved. No Reproduction Permitted. Email corrections/comments to MilitaryFactory at Gmail dot com.

Specifications for the
Sukhoi Su-17 / Su-20 / Su-22 (Fitter)
Ground Attack / Strike Fighter

Focus Model: Sukhoi Su-17M4 (Fitter-K)
Country of Origin: Soviet Union
Manufacturer: Sukhoi - Soviet Union / Russia
Initial Year of Service: 1970
Production: 2,867

Crew: 1

Length: 62.40 ft (19.02 m)
Width: 44.88 ft (13.68 m)
Height: 16.80ft (5.12 m)
Weight (Empty): 26,808 lb (12,160 kg)
Weight (MTOW): 42,990 lb (19,500 kg)

Powerplant: 1 x Lyulka AL-21F-3 turbojet engine generating 24,802lbs.

Maximum Speed: 718 mph (1,155kmh; 624 kts)
Maximum Range: 889 miles (1,430km)
Service Ceiling: 49,869 ft (15,200 m; 9.4 miles)
Rate-of-Climb: 45,275 feet per minute (13,800 m/min)

Hardpoints: 12
Armament Suite:
2 x 30mm Nudelman-Rikhter NR-30 cannons in leading edge wing roots.

10 to 12 hardpoints for up to 9,000lbs of mixed ordnance including conventional drop bombs, napalm, drag chute bombs, runway-defeating bombs, TV/Laser-guided bombs, rocket pods, gun pods, air-to-surface missiles and air-to-air missiles.

Su-7 (Fitter-A) - Base Fixed-Wing Interceptor Model on which the Su-17 is based on.

Su-7IG/ S-22I (Fitter-B) - Based on the Su-7BM production model; used in testing the swing-wing component.

Su-17 (Fitter-B) - Base production model; limited production; extended fuselage based on the Su-7U two-seat trainer; revised airframe with dorsal fuselage spine; increased internal fuel capacity; fitted with Lyulka AL-7F-1 engine; production from 1969 to 1973.

Su-17K (Fitter-B) - Egyptian Export Model Designation of the base Su-17.

Su-17M (Fitter-C) - Initial Production Model of note; fitted with Lyulka AL-21F-3 engine; revised nav-attack system; implementation of dual pitot vanes as well as AoA vane; brake parachute; positional shock cone; production from 1972 to 1975.

Su-20 (Fitter-C) - Export Designation of Su-17M production model.

Su-17M-28 - Developmental Airframe for testing AS-9 "Kyle" anti-radar missile.

Su-17MKG - Developmental Airframe for testing AS-10 "Karen" and AS-14 "Kedge" air-to-surface missiles.

Su-17R (Fitter-C) - Limited Production Reconnaissance Variant of the Su-17M production model.

Su-20R (Fitter-C) - Export Designation of Su-17R reconnaissance model.

Su-17M2 (Fitter-D) - Redesigned and extended nose assembly; undernose Doppler radar; laser rangefinder; improved and expanded avionics; production from 1974 to 1977.

Su-17M2D (Fitter-D) - Fitted with Tumansky R-29BS-300 series engine of 25,335lbf; revised rear fuselage; production from 1977 to 1978.

Su-22 / S-32M2K (Fitter-F) - Export Designation of Su-17M2D production model.

Su-17UM / S-52U (Fitter-E) - Two -Seat Conversion Trainer; based on the Su-17M2 production model; revised deeper fuselage; deletion of internal fuel capacity; portside cannon removed; enlarged vertical tail fin for improved longitudinal control at high AoA; production from 1976 to 1978.

Su-22U - Export Model Designation of Su-17UM two-seat trainer; fitted with Tumansky R-29 series engine.

Su-17M3 / S-52 (Fitter-H) - Additional fuel and avionics equipment; based on two-seat trainer sans the second cockpit; improved range; internal Doppler radar system; launch rails installed for AA-2 and AA-8 missiles; production from 1976 to 1981.

Su-22M / S-52K (Fitter-J) - Export Model Designation of the Su-17M3; fitted with Tumansky R-29 series engine; downgraded avionics.

Su-22M3 / S-52MK (Fitter-J) - Export Model Designation of Su-17M3 with Soviet Su-17M3 avionics in place.

Su-17UM3 / S-52UM3 (Fitter-G) - Improved Two-Seat Trainer; Su-17M3 avionics; production from 1978 to 1982.

Su-22UM3 (Fitter-G) - Export Model Designation of Su-17UM3 trainer; fitted with Tumansky R-29 engine.

Su-22UM3K (Fitter-G) - Export Model Designation of Su-17UM3 trainer; fitted with Lyulka AL-21 engine.

Su-17M4 - Upgraded avionics suite; improved laser rangefinder; Sirena radar-warning receiver; fuselage and dorsal air inlets for improved engine cooling; fixed shock cone; TV-guided ordnance compatibility; production from 1981 to 1988.

Su-22M4 / S-54K - Export Model Designation of Su-17M4 production model; production from 1983 to 1990.

Su-22M5 - Modernized Fitters with French/Russian-based equipment and systems; HOTAS; glass cockpit; improved avionics suite; Phazotron/Thomson-CSF radar system; sans laser rangefinder.

Armenia; Afghanistan; Algeria; Angola; Azerbaijan; Belarus; Bulgaria; Czech Republic; Czechoslovakia; East Germany; Egypt; Germany; Hungary; Iraq; Iran; Libya; North Korea; Peru; Poland; Russia; Slovakia; Soviet Union; Syria; Turkmenistan; Ukraine; Uzbekistan; Vietnam; Yemen