Photos from the personal collection of Kostas Panitsidis
Technical specifications Photos Video
The export Su-17M4 with the power plant of the AL-21F-3, improved avionics. Production of the Su-22M4 began in 1980 and lasted until 1990.
Su-22M4 (S-54K): The export Su-17M4 with the power plant of the AL-21F-3, improved avionics. Production of the Su-22M4 began in 1980 and lasted until 1990.
THREE-VIEW DRAWING
TECHNICAL SPECIFICATIONS
DESIGNER
|
OKB Sukhoi
|
---|---|
COUNTRY
|
Russia
|
TYPE
|
Fighter-Bomber
|
CREW
|
1
|
POWER-PLANT
|
One jet engine R-29Β-300
|
Thrust, kgf
|
1 x 11.500
|
DIMENSIONS
|
|
Length, m
|
18,86
|
Height, m
|
4,86
|
Wing span, m
|
-
|
- maximum
|
13,68
|
- minimum
|
10,025
|
Wing area, m2
|
-
|
- maximum
|
38,49
|
- minimum
|
34,45
|
WEIGHT
|
|
Empty aircraft, kg
|
10.445
|
Maximum take-off, kg
|
18.820
|
Internal fuel, kg
|
3.770
|
Fuel capacity in external tanks, kg: | - |
PERFORMANCE
|
|
Maximum speed, km/h
|
2.230
|
Max speed in low height, km/h
|
1.350
|
Range, km
|
-
|
- with external fuel tanks | 2.550 |
Combat range, km
|
590
|
Service ceiling, m
|
14.000
|
ARMAMENT | Two 30 mm cannons NR-30 (160 rounds) Warload - 4.000 kg in 8 hardpoints. Airtoair missile R-60, Airtosurface missile Kh-25MR, Kh-25MP. Bombs KAB-500. Bombs - free fall, guided, cluster, fire bombs, cannon pods etc. |