Photos from the personal collection of Kostas Panitsidis
Technical specifications Photos Video
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.
Su-22M (S-52K): Su-22 M equipped with missile Kh-28 and pods targeting "Metel-A"
The first flight of the prototype took place in 1976. During the period 1976 to 1981 were built more than 2,820 aircraft of all versions.
THREE-VIEW DRAWING
TECHNICAL SPECIFICATIONS
DESIGNER
|
OKB Sukhoi
|
---|---|
COUNTRY
|
Russia
|
TYPE
|
Fighter-Bomber
|
CREW
|
1
|
POWER-PLANT
|
One jet engine AL-21F-3
|
Thrust, kgf
|
1 x 11.200
|
DIMENSIONS
|
|
Length, m
|
19,02
|
Height, m
|
5,13
|
Wing span, m
|
-
|
- maximum
|
13,65
|
- minimum
|
10,02
|
Wing area, m2
|
-
|
- maximum
|
38,49
|
- minimum
|
34,45
|
WEIGHT
|
|
Empty aircraft, kg
|
11.800
|
Maximum take-off, kg
|
19.630
|
Internal fuel, kg
|
4.020
|
Fuel capacity in external tanks, kg: | 2.875 |
PERFORMANCE
|
|
Maximum speed, km/h
|
2.230
|
Max speed in low height, km/h
|
1.400
|
Range, km
|
1.520
|
- with external fuel tanks | 2.550 |
Combat range, km
|
-
|
Service ceiling, m
|
14.000
|
ARMAMENT | Two 30 mm cannons NR-30 (160 rounds). Warload - 3.600 kg in 10 hardpoints. Air-to-air missile R-60, Air-to-surface missile Kh-28, Kh-27PS, Kh-25MP, Kh-58U. Bombs KAB-500Kr. Bombs - free fall, guided, cluster, fire bombs, cannon pods UPK-23-250, pods KMGU-1 and KMGU-2 etc. |
PHOTOS Su-17M3 Fitter