.jpg "Su-17M Fitter Fighter-bomber. First flight: 1971 © Konstantinos Panitsidis")
In numbers Through the lens Video
NATO reporting name: Fitter C
izdeliye S-32M
Version produced in large numbers, which includes new engine AL-21F-3, increasing fuel capacity and upgraded electronics.
The first flight took place on December 28, 1971.
Configurations weapon Su-17 M: The rocket S-24 is intended primarily for challenging mobile and stationary armored targets, shelters etc. The production of the missile began in 1960. The missile is certified for use by other aircraft.
ZΒ-500 Napalm bomb
Bomb ZAB-500-400
Rocket launcher B-8M-1
FAB-250TS bombs
Combined transport fuel tanks PTB-800, and cannon pods UPK-23-250 with 250 rounds.
Combined reconnaissance pod - KKR.
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 | 1x9.600 |
| DIMENSIONS | |
| Length, m | 18,72 |
| Height, m | 4,85 |
| Wing span, m | - |
| - minimum | 13,65 |
| - maximum | 10,04 |
| Wing area, m2 | - |
| - minimum | 38,49 |
| - maximum | 34,45 |
| WEIGHT | |
| Maximum take-off, kg | 18.120 |
| Normal take-off, kg | - |
| Empty aircraft, kg | 9.800 |
| Internal fuel, kg | 2.980 |
| Weight of transported fuel with external tanks, l | 2.875 |
| Warload, kg | 3.000 |
| PERFORMANCE | |
| Maximum speed, km/h | 2.230 |
| Maximum speed in low height, km/h | 1.200 |
| Range, km | |
| - without external fuel tanks | 1.350 |
| - with external fuel tanks | 2.700 |
| Combat range, km | - |
| Service ceiling, m | 16.800 |
| ARMAMENT | Two 30 mm cannons NR-30 with 160 rounds. Number external hardpoints: 8. Transportation of weapons: R-60, Kh-23, Kh-25. Bombs - free fall, guided, cluster, fire bombs, cannon pods UPK-23-250, pods KMGU-1 and KMGU-2 etc. |
Photos Su-17M Fitter
