Sukhoi Zo-17UM3

Sukhoi Zo-17

LandUssr
TypeSovjet aanvalsvliegtuigen
Eerste vluchtvan 2 augustus 1966
Gebouwd2867

Fotogalerij van een Sukhoi Su-17UM3.

De Sukhoi Zo-17 (NAVO-rapporteringsnaam: Fitter) is een Sovjet-aanvalsvliegtuig ontwikkeld van de Sukhoi Su-7 jachtbommenwerper. Het genoot een lange carrière in Sovjet, later Russisch, dienst en werd wijd geëxporteerd aan communistische en Midden-Oosterse luchtmachten, onder namen Su-20 en Su-22.

Bron: Sukhoi Su-17UM3 op Wikipedia

Sukhoi Su-17UM3
FotograafOnbewust
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Su-17m fitter rond te lopen
FotograafEugeny Ivanov
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Sukhoi Su-17M3 Walk Around
FotograafSergey Zhabin
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Su-22 UM Walk Around
FotograafCees Hendriks
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Zie ook:

Tweede Wereldoorlog: de definitieve visuele geschiedenis van Blitzkrieg tot de atoombom (DK Definitive Visual Histories) - Amazon Kaart voor kaart van de Tweede Wereldoorlog (DK History Map by Map) - Amazon

Sukhoi Su-20 Fitter-C Walk Around
FotograafBurkhard Domke
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Sukhoi Su-22M4 Fitter-K Walk Around
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Sukhoi Su-17M4 Fitter K Walk Around
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De Sukhoi Zo-17UM3 is a two-seat, advanced operational trainer variant of the venerable Soviet Su-17 variable-sweep wing fighter-bomber (NATO designation “Fitter”). It was developed from the earlier Su-17UM, incorporating the improved avionics and systems of the single-seat Su-17M3 ground-attack aircraft.


Design and Role

Trainer Configuration:

  • Primary role is to provide advanced training and conversion for pilots transitioning to the high-performance Su-17/22 family of attack jets.
  • It features a tandem two-seat cockpit, with the instructor occupying the rear seat.
  • The aircraft utilizes a raised, deeper dorsal spine (similar to the single-seat Su-17M3) to accommodate additional avionics and fuel tankage, compensating for the weight and space taken up by the second cockpit.

Variable-Sweep Wings:

  • Like all Su-17 variants, the Su-17UM3 uses the signature variable-sweep outer wing panels, allowing for excellent low-speed handling (takeoff/landing) and high-speed performance (supersonic flight) in a single airframe.
  • The sweep angle can be configured between approximately 30° and 63°.

Operational Capability:

  • Although primarily a trainer, the Su-17UM3 retains significant combat capability, sharing the weapon hardpoints and weapon delivery systems of the single-seat variants.
  • It is typically powered by the Lyulka AL-21F-3 afterburning turbojet engine (unlike some export trainers, the Su-22UM3, which used the Tumansky R-29 engine).

General Specifications (Approximate, based on Su-17M3/UM3 data)

Feature Specificatie
Type Advanced Two-Seat Trainer / Fighter-Bomber
Bemanning 2 (Pilot and Instructor/Trainee)
Motor Lyulka AL-21F-3 Afterburning Turbojet
Max Speed Approx. Mach 1.7 (High Altitude) / Mach 1.1 (Sea Level)
Main Armament Two 30 mm Nudelman-Rikhter **NR-30** cannons
Payload Capacity Up to 4,000 kg (8,800 lbs) of ordnance (bombs, rockets, missiles, gun pods)
Wingspan (Unswept) Approx. 13.68 m (44 ft 11 in)
Lengte Approx. 19.02 m (62 ft 5 in)

Bekeken : 8825

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