Su-17M3 Fitter H (S-52, Su-19) Fighter-Bomber. First flight: 1976 © Konstantinos Panitsidis

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-22M equipped with missile Kh-28 and pods targeting "Metel-A" © Konstantinos Panitsidis  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

Su-17M3 Fitter © Konstantinos Panitsidis

 


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