In numbers Through the lens Video
NATO reporting name: Fitter H
Often referred to as: S-52, Su-19
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.
| Modifications: |
| Su-17M3-58-27: Flying laboratory for testing Kh-27PS and Kh-58U missiles. |
| Su-17M3P (S-52P): Modified version, capable of carrying Kh-27PS, Kh-58 anti-radar missiles, with "V'uga-17" targeting equipment. A number of Su-17M3 aircraft were modified to the level of the Su-17M3P. |
| Su-17M3P: Reconnaissance aircraft version with based on the Su-17M3. |
Three-view drawing

Technical specifications
| DESIGNER | OKB Sukhoi |
| COUNTRY | Russia |
| TYPE |
Fighter-bomber
|
| CREW | 1 |
| POWER-PLANT | One turbojet engine AL-21F-3 |
| Thrust, kgf | 1x11.200 |
| DIMENSIONS | |
| Length, m | 19,02 |
| Height, m | 5,13 |
| Wing span, m | - |
| - minimum | 13,68 |
| - maximum | 10,02 |
| Wing area, m2 | - |
| - minimum | 38,49 |
| - maximum | 34,45 |
| WEIGHT | |
| Maximum take-off, kg | 19.630 |
| Normal take-off, kg | - |
| Empty aircraft, kg | 11.800 |
| Internal fuel, l | 4.020 |
| Weight of transported fuel with external tanks, l. | 2.875 |
| Warload, kg | 3.600 |
| PERFORMANCE | |
| Maximum speed, km/h | 2.230 |
| Maximum speed in low height, km/h | 1.400 |
| Range, km | 1.520 (2.550) |
| Combat range, km | - |
| Service ceiling, m | 14.000 |
| ARMAMENT | Two 30 mm cannons NR-30 with 160 rounds. Number external hardpoints: 10. Transportation of weapons: 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