.jpg "Su-25SM Εγγύς υποστήριξης. Πρώτη πτήση: 1999 © Konstantinos Panitsidis")
In numbers Through the lens Video
Technical specifications
| DESIGNER | OKB Sukhoi |
| COUNTRY |
Russia
|
| TYPE | Attack aircraft |
| CREW | 1 |
| POWER-PLANT | Two turbojet engines R-195 |
| Thrust, kg | 2x4.500 |
| DIMENSIONS | |
| Length, m | 15,36 |
| Height, m | 4,80 |
| Wing span, m | 14,36 |
| Wing area, m2 | 33,70 |
| WEIGHT | |
| Maximum take-off, kg | 17.600 |
| Normal take-off, kg | 14.600 |
| Empty aircraft, kg | 9.500 |
| Internal fuel, kg | 5.000 |
| Weight of transported fuel with external tanks, kg | 2.000 |
| Warload, kg | 4.340 |
| - standard configuration, kg | 1.340 |
| PERFORMANCE | |
| Maximum speed (at high altitude), km/h | 1.004 |
| Maximum speed, sea level km/h | - |
| Maximum speed in low height, km/h | 975 |
| Range, km | - |
| Combat range, km | 1.850 |
| Service ceiling, m | 10.000 |
| Maximum overload, g | 6,5 |
| ARMAMENT | 30 mm two-barrel cannon GSh-30-2 with 250 rounds. Number external hardpoints: 10. Transportation of weapons: 8-10x500 ,250 kg bombs, 32x100 kg bombs, napalm tanks, rokets 8-10 ML UB-32-57 (320 (252)x57 mm) or 8-10 240 mm, packets UR S-5 (57 mm), S-8 (80 mm), S-24 (240-mm)xS-25 (340 mm). Air-to-air missile, Air-to-surface missile Kh-25ML, Kh-29L and S-25L. SPPU-22 pods with 23 mm cannon GSh-23L with 260 rounds. |
Photos Su-25SM
