| Název: Name: | Suchoj Su-17M2 | Sukhoi Su-17M2 |
| Originální název: Original Name: | Сухой Су-17М2 | |
| Kategorie: Category: | stíhací-bombardovací letoun | fighter-bomber aeroplane |
| Výrobce: Producer: | DD.MM.1975-DD.MM.1979 Dálněvýchodní strojírenský závod, Komsomolsk na Amuru | |
| Období výroby: Production Period: | DD.MM.1975-DD.MM.1979 | |
| Vyrobeno kusů: Number of Produced: | 268 | |
| První vzlet: Maiden Flight: | DD.MM.1973 (S-32M2) | |
| Osádka: Crew: | 1 | |
| Základní charakteristika: Basic Characteristics: | ||
| Vzlet a přistání: Take-off and Landing: | CTOL - konvenční vzlet a přistání | CTOL - conventional take-off and landing |
| Uspořádání křídla: Arrangement of Wing: | jednoplošník s měnitelnou geometrií křídla | monoplane with variable geometry wing |
| Uspořádání letounu: Aircraft Concept: | klasické | conventional |
| Podvozek: Undercarriage: | zatahovací | retractable |
| Přistávací zařízení: Landing Gear: | kola | wheels |
| Technické údaje: Technical Data: | ||
| Hmotnost prázdného letounu: Empty Weight: | 10445 kg | 23027 lb |
| Vzletová hmotnost: Take-off Weight: | ? kg | ? lb |
| Maximální vzletová hmotnost: Maximum Take-off Weight: | 18820 kg | 41491 lb |
| Rozpětí: Wingspan: | 13,681) m | 44ft 10,58in 1) |
| Délka: Length: | 18,868 m | 61ft 10,83in |
| Výška: Height: | 4,857 m | 15ft 11,22in |
| Plocha křídla: Wing Area: | 38,492) m2 | 414.3 2) ft2 |
| Plošné zatížení: Wing Loading: | ? kg/m2 | ? lb/ft2 |
| Pohon: Propulsion: | ||
| Kategorie: Category: | jednoproudový | turbojet |
| Počet motorů: Number of Engines: | 1 | |
| Typ: Type: | Ljulka AL-21F-3 (АЛ-21Ф-3), ťah 76,49 kN (109,83 kN s forsážou) | Lyulka AL-21F-3, thrust 17195 lbf (24692 lbf with afterburner) |
| Objem palivových nádrží: Fuel Tank Capacity: | 3770 kg | 8311 lb |
| Výkony: Performance: | ||
| Maximální rychlost: Maximum Speed: | 1350 km/h v ? m | 838.9 mph in ? ft |
| Cestovní rychlost: Cruise Speed: | ? km/h v ? m | ? mph in ? ft |
| Rychlost stoupání: Climb Rate: | 220 m/s | 43307.1 ft/min |
| Čas výstupu na výšku: Time to Climb to: | ? min do ? m | ? min to ? ft |
| Operační dostup: Service Ceiling: | 15400 m | 49869 ft |
| Dolet: Range: | ? km | ? mi |
| Maximální dolet: Maximum Range: | 2500 km | 1553.4 mi |
| Výzbroj: Armament: | 2 x 30mm kanón NR-30 (2x 80 nábojov) 4000 kg výzbroje na 8 závesníkoch - PL rakety R-60, R-3S - rakety Ch-23 - rakety Ch-25 - rakety Ch-28 (1 ks) - rakety S-25L (od roku 1979) - rakety S-25LD (od roku 1985) - bomby do kalibru 500 kg - bloky neriadených rakiet UB-32-57, UB-16-57UM, B-8M-1, S-25 (APU-68U) - strelecký kontajner UPK-23-250, SPPU-22-01 - kazetový kontajner KMGU-1, KMGU-2 - zápalné nádrže ZB-500, ZB-500Š | 2 x 30mm gun NR-30 (2 x 80 rounds) 8818 lb of ordnance, 8 hardpoints: - AA missiles R-60, R-3S - missiles Kh-23 - missiles Kh-25 - missiles Kh-28 (1 pc) - missiles S-25L (from 1979) - missiles S-25LD (from 1985) - bombs to 500 kg calibre - unguidet missile containers UB-32-57, UB-16-57UM, B-8M-1, S-25 (APU-68U) - gun container UPK-23-250, SPPU-22-01 - cluster container KMGU-1, KMGU-2 - incendiary tanks ZB-500, ZB-500Sh |
| Uživatelské státy: User States: | | |
| Poznámka: Note: | Zhrnutie informácií o vývoji typovej rady v článku Kód NATO: Fitter-D Exportná verzia: Su-22 (S-32M2K) 1) pri nastavení krídla v uhle 30°, 10,025 pri nastavení v uhle 63° 2) pri nastavení krídla v uhle 30°, 34,45 m2 pri nastavení v uhle 63° | Information about development in article NATO code: Fitter-D Export version: Su-22 (S-32M2K) 1) pri nastavení krídla v uhle 30°, 10,025 pri nastavení v uhle 63° 2) pri nastavení krídla v uhle 30°, 34,45 m2 pri nastavení v uhle 63° |
| Zdroje: Sources: | MARKOVSKIJ Viktor, PRICHODČENKO Igor: Istrebiteľ-bombardirivščik Su-17; Eksprint 2003+ ISBN 5-94038-037-9 | |
Suchoj Su-17M2 [kód NATO: Fitter-D]
Sukhoi Su-17M2 / Сухой Су-17М2
Su-17M2(S-32M2, S-42)(Su-17M2 (S-32M2, S-42)) - basic version. Compared to the previous version Su-17M1, it has an extended nose section by 200 mm and a slightly enlarged cabin. The aircraft is equipped with the FON-1400 ("Фон-1400) laser rangefinder, ASP-17S (АСП-17С) optical sight, and PBK-Z-17S (ПБК-3-17С) combined sight. The fuel tank volume is increased by 200 litres. First flight in October 1973, produced in 1975-1979. Officially accepted into armament on 3 February 1976
- Su-17M2-D (Su-17M2-D) - elaborated (doled), differed by the use of the DISS-7 (Su-17M2-D) Doppler velocity and angle of attack sensor and the DISS-7 (DISS-7) missile guidance apparatus Ch-23(Х-23) located in the container.
- The Su-17M2R (Су-17М2Р) - reconnaissance variant, differed by the possibility of using an under-hung KKR-1/54 (ККР-1/54) reconnaissance container and an active electromagnetic interference generating station.
- Su-17UM2 - two-seat training version
- Su-22 - export version (Libya, Peru, Syria, Iraq)
- Su-22UM2 - export version
- Su-17M2-D (Su-17M2-D) - elaborated (doled), differed by the use of the DISS-7 (Su-17M2-D) Doppler velocity and angle of attack sensor and the DISS-7 (DISS-7) missile guidance apparatus Ch-23(Х-23) located in the container.
- The Su-17M2R (Су-17М2Р) - reconnaissance variant, differed by the possibility of using an under-hung KKR-1/54 (ККР-1/54) reconnaissance container and an active electromagnetic interference generating station.
- Su-17UM2 - two-seat training version
- Su-22 - export version (Libya, Peru, Syria, Iraq)
- Su-22UM2 - export version
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http://www.airwar.ru/enc/fighter/su17m2.html
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Diskuse
According to Russian sources and information from pilots on Russian discussion forums, the Su-17M2R variant did not exist. All serial Su-17M2 aircraft whose serial numbers ended in zero or five had, like the Su-7BM/BKL/BMK, Su-17, Su-17M aircraft, an additional shaft behind the nose gear shaft, which contained a single AFA-39 camera for perpendicular imaging. The online aviation encyclopedia Ugolok Neba and others lists some outdated information for the Su-17/20/22, probably taken from the publication by Yefim Gordon and Dmitry Komissarov "Sukhoi Su-7/Su17 published by Midland Publishing in 2011, although it is not listed among the sources. I'm basing it on the most recent comprehensive monograph on the Su-17 aircraft, published in 2011 and 2012 in Aviacia i kosmonavtika vchera, segodnya i zavtra by Viktor J. Markovsky and Igor V. Prikhodchenko. It states in issue 5 of 2012 that the KKR container was developed by the P.O. Sukhoi design bureau itself and that it was originally intended for export variants only. The first flight tests on the Su-20 were conducted in 1975. It was only in the late 1970s that it was decided to use it on the Su-17M3. A new version of the container was tested first on the Su-22 (export version Su-17M2) in 1977 and on the Su-17M3 and its export version Su-22M in 1979. From 1979 ( 1980?), the reconnaissance variant Su-17M3R, later Su-17M4R, and the export Su-22MR, Su-22M3R and Su-22M4R were also produced. If the customer wished, these aircraft were directly delivered in the reconnaissance variant (for the Soviet and Czechoslovak air forces), but all aircraft could be converted by the services to the fighter-bomber version and vice versa, as all aircraft already had built-in wiring for container control. The Su-17M2R variant is not mentioned in the monograph, as their production was discontinued in 1977.
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