In numbers Through the lens Video
NATO reporting name: Flanker E
The Su-35 is a singleseat super-agile multirole fighter powered by two AL-31FP 12,500-kgf thrust vector-controlled (TVC) engines.
The first AL-31F-powered Su-35 prototype (Su-27M) flight took place on 28 June, 1988. In 1996, the first several Su-35s were fielded with the Russian Air Force. In 1996, one of the Su-35 prototypes (side number 711) was fitted with thrustvectored engines for the very first time.
Its maiden flight in its new capacity was made on 2 April, 1996. Su-35's derivative is the Su-35UB twin-seat super-agile multirole fighter whose prototype first flew on 7 August, 2000.
The Su-35 has two widely spaced AL-31F turbofan engines, with afterburner, and 12.500 kgf afterburning thrust each, with thrust-vectoring nozzle control.
Equipment aircraft: A pulse-Doppler radar N011/Zhuk-27 with multiple versions arrangements: of a simple and distinct facet capacity, following and avoiding terrain-relief, mapping, weather radar, moving ground target trace and tracking, and air-to-air firing version optimized for firing bellow the flying of the aircraft.
Electro-optical OEPS-27 system with an OLS-jamming maximum radius range 50 km which covers the rear hemisphere of the aircraft. The radar provides: Detection range 400 km, Range for target jamming 100+ km, Number of detected and tracked targets: 15, Number of simultaneous attacks against targets: 6.
Three-view drawing
Technical specifications
| DESIGNER | OKB Sukhoi |
| COUNTRY |
Russia
|
| TYPE | Multipurpose fighter |
| CREW | 1 |
| POWER-PLANT | Two turbofan engines ΝPO Saturn Lyl'ka AL-31F |
| Thrust, kgf | 2x12.500 |
| DIMENSIONS | |
| Length, m | 22,18 |
| Height, m | 6,35 |
| Wing span, m | 14,70 |
| Wing area, m2 | - |
| WEIGHT | |
| Maximum take-off, kg | 34.000 |
| Normal take-off, kg | 25.700 |
| Empty aircraft, kg | - |
| Internal fuel, kg | - |
| Warload, kg | 8.000 |
| PERFORMANCE | |
| Maximum speed (at high altitude}, km/h | 2.440 |
| Maximum speed in low height, km/h | 1.400 |
| Service ceiling, m | 18.000 |
| Rate of climb, m/min | - |
| Range, km | 4.000 |
| Maximum overload, g | 10 |
| ARMAMENT | 1x30 mm cannon GSh-301 with 150 rounds. Number external hardpoints: 12. Transportation of weapons: Air-to-surface missile Kh-29T/L, Kh-25ML, Kh-31A/P, Kh-59M and S-25L. Air-to-air missile 8x R-27RE, R-27TE, R-77 or R-60M, R-73M, R-73. Bombs KAB-500KR/L. Free fall bombsFAB-500, FAB-250, OFAB-100. Cluster bombs, ECM pods. Rokets S-8, S-13, S-25. |
Photos Su-35 Flanker E, Aviation Museum VVS, Monino 2007 (Russia).
