Suchoj Su-17UM [kód NATO: Fitter-E]

Sukhoi Su-17UM / Сухой Су-17УМ
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Název:
Name: 		Suchoj Su-17UM Sukhoi Su-17UM
Originální název:
Original Name: 		Сухой Су-17УМ
Kategorie:
Category: 		cvičný letoun trainer aeroplane
Výrobce:
Producer:		 DD.MM.1975-DD.MM.1978 Dálněvýchodní strojírenský závod, Komsomolsk na Amuru /
Období výroby:
Production Period: 		DD.MM.1975-DD.MM.1978
Vyrobeno kusů:
Number of Produced: 		75
První vzlet:
Maiden Flight: 		15.08.1975 S-52U
Osádka:
Crew: 		2
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: 		10900 kg 24030 lb
Vzletová hmotnost:
Take-off Weight: 		14520 kg 32011 lb
Maximální vzletová hmotnost:
Maximum Take-off Weight: 		18510 kg 40808 lb
Rozpětí:
Wingspan: 		13,681) m 44ft 10,58in 1)
Délka:
Length: 		17,34 m 56ft 10,67in
Výška:
Height: 		5,13 m 16ft 9,96in
Plocha křídla:
Wing Area: 		38,491) m2 414.3 1) 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 o tahu 76,49 kN / 109,83 kN s přídavným spalováním Lyulka AL-21F-3, thrust 17195 lbf / 24692 lbf with afterburner
Objem palivových nádrží:
Fuel Tank Capacity: 		3720 l 818 Imp gal / 983 US gal
Výkony:
Performance: 		 
Maximální rychlost:
Maximum Speed: 		1350 km/h v 0 m 838.9 mph in 0 ft
Cestovní rychlost:
Cruise Speed: 		? km/h v ? m ? mph in ? ft
Rychlost stoupání:
Climb Rate: 		? m/s ? ft/min
Čas výstupu na výšku:
Time to Climb to: 		? min do ? m ? min to ? ft
Operační dostup:
Service Ceiling: 		15400 m 50525 ft
Dolet:
Range: 		1200 km 745.6 mi
Maximální dolet:
Maximum Range: 		2000 km 1242.7 mi
Výzbroj:
Armament: 		1x kanon NR-30 ráže 30 mm, 80 nábojů

3000 kg podvěšené výzbroje na 8 závěsnících:
2x Ch-25
2x R-60
raketnice UB-32A s 32 neřízenými raketami S-5 ráže 57 mm
raketnice B-8M-1 s 20 neřízenými raketami S-8 ráže 80 mm
kontejner SPPU-22 s kanonem GŠ-23L
rakety S-24 ráže 240 mm
rakety S-25 ráže 250 mm
500kg pumy
...		 1x 30 mm NR-30 cannon, 80 rounds

6614 lb of ordnance, 8 hardpoints:
2x Kh-25
2x R-60
UB-32A rocket pods with 32 S-5 57 mm unguided rockets
B-8M-1 rocket pods with 20 S-8 80 mm unguided rockets
SPPU-22 pods with GSh-23L cannon
240 mm S-24 rockets
250 mm S-25 rockets
1102 lb bombs
...
Uživatelské státy:
User States:





Poznámka:
Note: 		1) šípovitost 30°, 10,03 m při šípovitosti 63°
2) šípovitost 30°, 34,50 m2 při šípovitosti 63°		 1) at 30° sweep; 32ft 10,87in at 63° sweep
2) at 30° sweep; 371.35 ft2 at 63° sweep
Zdroje:
Sources: 		Gordon, Yefim. Sukhoi Su-7/-17/-20/-22: Soviet Fighter and Fighter-Bomber Family. Midland Publishing, Hinckley 2004. ISBN 1-85780-108-3.
ruslet.webnode.cz
URL : https://www.valka.cz/Suchoj-Su-17UM-kod-NATO-Fitter-E-t41179#559632 Version : 0
History:



The Su-17UM or Su-17UM-2D (export designation Su-22UM-2D) is the first trainer type derived from the Su-17/20/22 development series. It was based on the single-seat Su-17M-2D, with some elements of the later Su-17M3. The sloping nose and the possibility of using two types of power units (Ljulka Al-21F for VVS aircraft and Tumanskiy R-29BS for export aircraft) are taken from it.


The conversion was carried out by extending the nose behind the existing cockpit and installing a second cockpit with a complete set of control instruments. The overlap of the instructor's cockpit is in the outline of the forward cockpit, with a glazed spacer sandwiched between the two hinged sections, overlapping the bulkhead (in which two glazed portholes have been cut to allow a view of the forward cockpit from behind) behind the ejection seat of the balanced pilot and the hydraulic forward cockpit hinging system. This mezzanine design is taken from the Su-7U. A hinged periscope is placed in the instructor's overlay for viewing the forward hemisphere of the aircraft (due to the need for unobstructed vision, the mirror from the forward cockpit overlay is removed). The ejection seats in both cockpits are of the standard type, more precisely K-36 of the first production series.


The fuselage carries the original vertical tailplane of the low type from the Su-17M-2D. Weight compensation of the second cockpit is made by removing the left NR-30 gun and its ammunition magazines. The other combat capabilities of the aircraft are retained according to Su-17M-2D. Later production versions were upgraded to replace most of the original Su-17M-2D type instrumentation (avionics and weapons systems) with those of the Su-17UM-3 (Su-22UM-3K) aircraft, which reduced the maintenance costs of the jointly serving Su-17UM-2D and Su-17UM-3 trainers.
URL : https://www.valka.cz/Suchoj-Su-17UM-kod-NATO-Fitter-E-t41179#165566 Version : 0
A summary of the history of the entire Sukhoi Su-17/20/22 development series can be found in this article
URL : https://www.valka.cz/Suchoj-Su-17UM-kod-NATO-Fitter-E-t41179#179467 Version : 0
Su-17UM aircraft, low rudder, missing lower keel and split nose gear door.


Source. Prikhodchenko.

Suchoj Su-17UM [kód NATO: Fitter-E] -


URL : https://www.valka.cz/Suchoj-Su-17UM-kod-NATO-Fitter-E-t41179#527210 Version : 0
The development of the Su-17UM was exactly the opposite than in the Darkfold. First was developed a two-seat version and the next from her single-seat Su-17M3. The length of the fuselage for both versions is the same.

Source: Victor J. Markovskij, Igor In. Prichodčenko: Istrebitěl-bombardirovščik Su-17, Aviacia i kosmonavtika yesterday, segodnya i zavtra no 5 - 7,9 - 11/2011, 1,4 - 8/2012.
URL : https://www.valka.cz/Suchoj-Su-17UM-kod-NATO-Fitter-E-t41179#566540 Version : 0
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