- Sukhoi Su-17
infobox Aircraft
name = Su-17/-20/-22
caption = Su-20 in the markings of 7th Bombing-Reconnaissance Regiment of Polish Air Force
type = Fighter-bomber
national origin = USSR
manufacturer =Sukhoi OKB
first flight =1 July 1969
introduction = 1970
retired = 1998 (Russia)
status =
primary user =Russian Air Force Egyptian Air Force Polish Air Force
more users =
produced = 1969-1990
number built = 2,867
unit cost =
developed from =Sukhoi Su-7
variants with their own articles =The Sukhoi Su-17 (
NATO reporting name : Fitter) was a Sovietattack aircraft developed from theSukhoi Su-7 fighter-bomber . It enjoyed a long career in Soviet/Russian service and was widely exported toEastern Bloc and Middle Eastern air forces.Development
Seeking to improve low-speed and takeoff/landing performance of the Su-7B fighter-bomber, in 1963 the Sukhoi OKB with input from
TsAGI created avariable geometry wing technology demonstrator. The Su-7IG (internal designation S-22I, NATO designation Fitter-B), converted from a production Su-7BM, had fixed inner portions of the wing with movable outer segments which could be swept to 28°, 45°, or 62°.cite book|last=Green|first=W|coauthors=Swanborough, G|year=2001|title=The great book of fighters|edition=|publisher=MBI Publishing|location=|id=ISBN 0760311943] A fixed inner wing simplified construction, allowing the manufacturer to retain the Su-7 landing gear and avoiding the need for complex pivoting underwing hardpoints, and it minimized the shift in thecenter of pressure relative to thecenter of mass with change in wing sweep.cite web|url=http://sukhoi.org/planes/museum/su17/|title=Sukhoi Su-17|work=Sukhoi Company Museum|accessdate=2007-04-15] The new wing also had extensive leading-edge slats and trailing-edge flaps. Su-7IG first flew on2 August 1966 with V. S. Ilyushin at the controls, becoming the first Soviet variable geometry aircraft. Testing revealed that takeoff and landing speeds had decreased by 50-60 km/h (27-32 knots, 31-37 mph) compared to the conventional Su-7.The production aircraft was named Su-17 (NATO designation Fitter-C, factory designation S-32) and was unofficially dubbed "Strizh" (Стриж,
martlet ) in service. Aside from the new wing, it differed from its predecessor Su-7 in having a new canopy and a dorsal fuselage spine for additional fuel and avionics. Su-17 first flew on1 July 1969 with E. K. Kukushev at the controls.A total of 2,867 Su-17 and its variants were built, of which 1,165 were exported to 15 nations worldwide.
Operational history
The Su-17 entered service with
Soviet Air Force in 1970. The aircraft was extensively used by both the Soviets and the government Afghanistan forces during theSoviet invasion of Afghanistan . High-altitude airfields and hot dusty climate created unique operational challenges. In the summer, the takeoff roll of the Su-17 increased 1.5-fold and landings frequently ended with burst tires and brake fires. Avionics failures were common due to heat and sand contamination. However, the AL-21F engine proved tolerant of routine ingestion of sand and sand-contaminated fuel and by 1985 the combat readiness of the Su-17 fleet exceeded that of theSukhoi Su-25 and the helicopters.cite journal|author=Markovskiy, Viktor|title=Жаркое Небо Афганистана|language=Russian|year=2000|journal=Техника - Молодежи] The first-series Su-17s were quickly replaced with more capable Su-17M3 and Su-17M4. Despite its durability and payload, the aircraft proved ill-adapted for combat in the mountainous terrain due to high attack speeds, low maneuverability, and the need to stay out of range ofanti-aircraft artillery due to lack of significant armor protection (although external armor was added around the engine, hydraulics, and fuel systems based on damage analysis, this was still insufficient compared to dedicated close air support Su-25s). The appearance of MANPADS such as the Soviet-madeStrela 2 (smuggled from Egypt), the BritishBlowpipe missile , and the AmericanFIM-43 Redeye and laterFIM-92 Stinger , presented a new threat and forced Su-17s to even higher operational altitudes. Revised tactics and retrofit of up to 12 flare dispensers which fired automatically during the attack run proved effective, and in 1985 only one Soviet Su-17 was lost to ground fire. Forced to operate 3500-4000 m (11,500-13,000 ft) above ground, Su-17s shifted from using unguided rockets to bombs, includingthermobaric weapon s, while Su-25s were tasked with precision strikes. Towards the end of the war, the Su-17 force was partially replaced by theMikoyan-Gurevich MiG-27 s in order to perform operational testing of the new fighter-bomber. Throughout the war, Afghani forces utilized Su-22s, three of which were shot down while operating in the vicinity ofPakistan aerospace by PakistaniF-16 Fighting Falcon s. The pilots responsible for the kills were F/L A Hameed Qadri, F/L Badr-ul-Islam and F/L Khalid Mahmood. [ [http://www.pafcombat.com/aerial-kills/paf-kills-afghan-war.htm combat armed force paf voyage at pafcombat.com ] ]Export variants of the Su-17 were also used in combat by
Libya andIraq . Two Libyan aircraft were shot down in the Gulf of Sidra incident byUS Navy F-14 Tomcat s on19 August 1981 . More were likely lost by Iraq during theIran–Iraq War in the 1980s, and six more were destroyed byUSAF aircraft in the1991 Gulf War .Fact|date=April 2007In a move to eliminate single engine strike aircraft from its inventory, The
Russian Air Force has retired its last Su-17M4 along with its fleet of MiG-23/27s in 1998. Around 550 remain in service with other nations.During the 1995 border war between Peru and Ecuador, two Peruvian Su-22s were shot down by Ecuadorian Mirage F-1s, killing both Peruvian pilots.
Variants
"Sources";Su-7IG (S-22I, Fitter-B):Su-7BM variable geometry wing demonstrator.;Su-17 (S-32, Fitter-B):Limited production run based on the longer fuselage of the two-seat Su-7U trainer, with bulged dorsal spine for extra fuel (4550 L/1,200 U.S. gal total). Retained Su-7's Lyulka AL-7F-1 engine. Manufactured 1969-1973.;Su-17K - export version of the Su-17 for Egyptian Air Force;Su-17M (S-32M, Fitter-C):First major production version, introduced Lyulka AL-21F-3 engine, twin
pitot tubes, new navigation and attack computer (retaining Su-7BMK's SRD-5M rangingradar ),angle of attack vane, single brake parachute. Variable-position intake centerbody providing maximum speed of Mach 2.1. First flight28 December 1971 with V. S. Soloviev at the controls. The export version was designated Su-20, first flying15 December 1972 with A. N. Isakov at the controls. Manufactured 1972-1975, entered service in 1973. Exported to Egypt, Poland, and Syria.;Su-17M-28:Testbed for Kh-28 (AS-9 Kyle) anti-radiation missile;Su-17MKG:Testbed for Kh-25 (AS-10 'Karen') and Kh-29 (AS-14 'Kedge') missiles;Su-17R:Small number of Su-17M aircraft equipped to carryreconnaissance pods. Equivalent export version designated Su-20R.;Su-17M2 (S-32M2, Fitter-D):Nose extended 38 cm (15 in), deleting ranging radar and 'drooping' to improve pilot visibility. Fon-1400laser rangefinder /marked-target seeker (LRMTS). ASP-17 and PBK-3-17s aiming avionics. RSBN-6S short-range navigation andinstrument landing system . Undernose fairing for DISS-7 Doppler navigationradar . First flight20 December 1973 with V. S. Ilyushin at the controls. Manufactured 1974-1977, entered service in 1975.;Su-17M2D:Test-fit of the Tumansky/Khatchaturov R-29BS-300 engine (shared with someMiG-23 s), with 112.7 kN (25,335 lbf) afterburning thrust, in a bulged rear fuselage. Due to lack of performance advantage and decreased range due to higher fuel consumption, it was decided to offer this engine as an export version only. First flight31 January 1975 with A. N. Isakov at the controls. The export variant was designated Su-22 (factory code S-32M2K, NATO Fitter-F), manufactured 1977-1978.;Su-17UM (S-52U, Fitter-E):First two-seat trainer version, based on the Su-17M2, but with a different, deeper fuselage with windscreen moved forward; same length as the original Su-17M. Internal fuel capacity reduced and port cannon deleted, but retained full avionics and armament. First flight15 August 1975 with V. A. Krechetov at the controls. Test flights revealed longitudinal instability at high angles of attack which was remedied by enlarging the tail fin. Export version with the R-29 engine was designated Su-22U. Manufactured 1976-1978, entered service in 1976.;Su-17M3 (S-52, Fitter-H):Based on the revised airframe of the Su-17UM, but with an avionics bay and an additional fuel tank in place of the rear cockpit, increasing the internal fuel capacity to 4850 l (1,280 U.S. gal). Doppler radar moved internally, removing the fairing. 'Klen-P' laser rangefinder/target designator. A launch rail for K-13 (AA-2 'Atoll') or R-60 (AA-8 'Aphid') was added between the two existing pylons on each wing. First flight30 June 1976 with V. A. Krechetov at the controls. Export version with the R-29 engine and downgraded avionics (equivalent to Su-17M2) was designated Su-22M (factory designation S-52K, NATO Fitter-J) and first flew on24 May 1977 with E. S. Soloviev at the controls. An export version with Su-17M3 avionics was designated Su-22M3 (factory S-52MK). Su-17 manufactured 1976-1981, Su-22M manufactured 1978-1984. Su-17M/Su-22M/Su-22M3 was the most numerous variant with almost 1,000 built.;Su-17UM3 (S-52UM3, Fitter-G):Revised trainer with the same avionics suite as the Su-17M3. First flight21 September 1978 with Yu. A. Yegorov at the controls. The export version was designated Su-22UM3 with R-29 engine, and Su-22UM3K with the AL-21 engine. Manufactured 1978-1982.;Su-17M4 (S-54, Fitter-K):Final production version with considerably upgraded avionics, including RSDN navigation (similar toLORAN ), beacon navigation,inertial navigation , a more powerful (Klyon)'Kлён-54' laser rangefinder, radio compass, and SPO-15LE ('Sirena') radar-warning system. Additional fuselage inlets (including ram-air inlet at the base of the fin) to improve engine-cooling air flow, fixed air intake shock cone. Many aircraft were equipped for the use of TV-guided missiles andBA-58 Vjuga pod foranti-radiation missile s. AL-21F-3 engine. Export version was designated Su-22M4 (factory S-54K). First flight19 June 1980 with Yu. A. Yegorov at the controls. Su-17M4 was manufactured 1981-1988, Su-22M4 was manufactured 1983-1990.;Su-22M5:A Russian-French upgrade package offered for existing aircraft with modernized cockpit,HOTAS , improved avionic systems. Deletes the laser rangefinder in favor ofPhazotron /Thomson-CSF 'Phathom' radar.Operators
; ARM: Many in the
Armenian Air Force , but the exact number is unknown.;AFG : More than 70 were sent to theAfghan Air Force from 1982, including 45 Su-22M-4 delivered from 1984.; DZA: TheAlgerian Air Force operated 32, although none remain in service.; ANG: ThePeople's Air and Air Defence Force of Angola operates 22 Su-22 variants.; AZE: TheAzerbaijan Air Force operates 2 Su-17.; BLR: TheBelarusian Air Force inherited Su-17s from the Soviet Air Force, but none remain in service.; BUL: TheBulgarian Air Force operated 18 Su-22M4 and 3 Su-22UM aircraft, but none remain in service.; CZE: TheCzech Air Force inherited 31 Su-22M-4 and 5 Su-22UM-3K. All were retired in 2002 [ [http://www.scramble.nl/cz.htm Info about Czech air force] ] . The Czech Su-22 aircraft were used inxXx movie.; CZS: Czechoslovak Su-22 (49 Su-22M-4 and 8 Su-22UM-3K in 1992) inventory was split between the Czech Republic and Slovakia in 1993.; GDR: The Air Forces of the National People's Army operated the Su-22 until unification, when they were passed on to theLuftwaffe .; EGY: TheEgyptian Air Force operated 48 of Su-20/22 aircraft, although all have been withdrawn, being replaced byF-4 Phantom II andF-16 Fighting Falcon s in their role.; GER: A number of Su-22 aircraft were inherited from East Germany, although these did not serve in theLuftwaffe ,but some of them have been painted withLuftwaffe color scheme for test and evaluation.; HUN: TheHungarian Air Force maintained 12 Su-22M3 and 3 Su-22UM-3 aircraft from 1983. Two single seat and one training aircraft crashed. Withdrawn from service in 1997. ; IRQ: TheIraqi Air Force received a number of Su-22 models, of which some were taken by Iran in 1991. None survived the2003 invasion of Iraq by the United States.; IRN: TheIslamic Republic of Iran Air Force operated a number of various Su-20 and Su-22 aircraft through the 1980s and 1990s, including examples flown to Iran from Iraq in 1991. While apparently non-operational, many remain in reserve or stored status.; LBA: TheLibyan Air Force operated as many as 90 Su-22, with around 40 Su-22M3 and Su-22UM3K aircraft currently in service.; PRK: As many as 30 may remain operational with theKorean People's Army Air Force .; PER: TheAir Force of Peru acquired 35 Su-22M, Su-22M3, and Su-22UM3, with as many as 20 remaining on inventory, though operational status is uncertain.; POL: ThePolish Air Force remains a major operator, with 48 Su-22M4K and Su-22UM3K aircraft in service of 137 delivered. All Polish Su-22 will be retired before 2012.; RUS: TheRussian Air Force inherited significant numbers of Soviet Su-17 aircraft, but has withdrawn the type from service.; SVK: The Air and Air Defense Forces inherited 18 Su-22M-4 and 3 Su-22UM-3K aircraft from Czechoslovakia in 1993, with current status uncertain.; USSR: Soviet Union Su-22s were split between post-USSR countries.
*Soviet Air Force
*Soviet Naval Aviation ; SYR: 60 Su-22 aircraft serve with theSyrian Air Force .; TKM: A number of Su-17 aircraft were inherited by theMilitary of Turkmenistan , but current status is unknown.; UKR: 40 Su-17 aircraft were inherited from the Soviet Union and are now retired from service.; UZB: A number of Su-17 aircraft were inherited by theMilitary of Uzbekistan , but current status is unknown.; VIE: Around 60 Su-22 examples serve with theVietnam People's Air Force .; YEM: 50 Su-22 have served with theYemen Air Force , with a number remaining active.pecifications (Su-17M4)
Aircraft specification
plane or copter?=plane
jet or prop?=jet
ref=Sukhoicite web|author=Sukhoi|title=Su-22M4|url=http://sukhoi.org/planes/military/su22m4/lth/|accessdate=2007-04-15]
crew=One
length main=19.02 m
length alt=62 ft 5 in
span main=
**Spread: 13.68 m (44 ft 11 in)
**Swept: 10.02 m
span alt=32 ft 10 in
height main=5.12 m
height alt=16 ft 10 in
area main=
**Spread: 38.5 m² (415 ft²)
**Swept: 34.5 m²
area alt=370 ft²
empty weight main=12160 kg
empty weight alt=26,810 lb
loaded weight main=16400 kg
loaded weight alt=36,155 lb
max takeoff weight main=19430 kg
max takeoff weight alt=42,835 lb
more general=Fuel capacity: 3770 kg (8,310 lb)
engine (jet)=Lyulka AL-21 F-3
type of jet=afterburningturbojet
number of jets=1
thrust main=76.4 kN
thrust alt=17,185 lbf
afterburning thrust main=109.8 kN
afterburning thrust alt=24,675 lbf
max speed main=
**Sea level: 1400 km/h (755 knots, 870 mph)
**Altitude: 1860 km/h
max speed alt=1,005 knots, 1,155 mph, Mach 1.7
range main=
**Combat: 1150 km (620 nm, 715 mi) in hi-lo-hi attack with 2,000 kg (4,410 lb) warload
**Ferry: 2300 km
range alt=1,240 nm, 1,430 mi
ceiling main=14200 m
ceiling alt=46,590 ft
climb rate main=230 m/s
climb rate alt=45,275 ft/min
loading main=443 kg/m²
loading alt=90.77 lb/ft²
thrust/weight=0.68
more performance=
*G-force limit: 7
*Airframe lifespan: 2,000 flying hours, 20 years
armament=
* 2× 30 mmNudelman-Rikhter NR-30 cannon, 80 rounds per gun
* Two underwing launch rails for R-60 (AA-8 'Aphid')air-to-air missile s for self-defense
* Up to 4000 kg (8,820 lb) on ten hardpoints (three under the fixed portion of each wing, four on the fuselage sides), including free-fall bombs, rocket pods,cluster bomb s, SPPU-22-01cannon pods with traversable barrels, ECM pods,napalm tanks, andnuclear weapon s. Current aircraft compatible with Kh-23 (AS-7 'Kerry'), Kh-25 (AS-10 'Karen'), Kh-29 (AS-14 'Kedge'), and Kh-58 (AS-11 'Kilter') guided missiles as well as electro-optical andlaser-guided bomb s.ee also
aircontent
related=
*Sukhoi Su-7 similar aircraft=
*A-7 Corsair II
*SEPECAT Jaguar
*Soko J-22 Orao
*Nanchang Q-5 lists=
*List of military aircraft of the Soviet Union and the CIS
*List of fighter aircraft References
External links
* [http://scalemodels.ru/modules/photo/viewcat_cid_257.html Walkaround Su-22M4]
* [http://www.warfare.ru/?catid=255&linkid=1603 from Russian Military Analysis]
* [http://www.fas.org/man/dod-101/sys/ac/row/su-17.htm from FAS]
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