In numbers Through the lens Video
NATO reporting name: Fulcrum
A single-seat supersonic multipurpose fighter, a modification of the MiG-29M light front-line fighter (number 156) and is a flying laboratory for testing RD-33 engines with an all-angle thrust vector deviation - the so-called KLIVT system, developed by the St. V.Ya. Klimov.
Three-view drawing
Technical specifications
| DESIGNER | OKB MiG |
| COUNTRY | Russia |
| TYPE |
Multipurpose fighter-bomber
|
| CREW | 1 |
| POWER-PLANT | Two turbofan bypass engines RD-33MK2 |
| Thrust, kgf | 2x8.800 |
| DIMENSIONS | |
| Length, m | 15,95 |
| Length+Pitot, m | 17,32 |
| Height, m | 4,73 |
| Wing span, m | 11,36 |
| Wing area, m2 | 38,06 |
| LANDIG GEAR | Retractable landing gears with a double nose wheel and a single-wheel system on the main gears. |
| Wheel base, m | 3,60 |
| Wheel track, m | 3,1 |
| WEIGHT | |
| Maximum take-off, kg | 22.300 |
| Normal take-off, kg | 16.680 |
| Empty aircraft, kg | 11.600 |
| Internal fuel, kg | - |
| Weight of transported fuel with external tanks, kg | - |
| Warload, kg | 4.500 |
| PERFORMANCE | |
| Maximum speed, km/h | 2.500 |
| Maximum speed in low height, km/h | 1.500 |
| Range, km | 2.000 |
| Service ceiling, m | 19.200 |
| Rate of climb, m/min | 19.200 |
| Maximum overload, g | 9 |
| ARMAMENT | One 30 mm cannon GSh-301 with 150 rounds. Number external hardpoints: 9. |
Photos MiG-29OVT
Video
MiG-29OVT - MAKS-2007. Video: © Konstantinos Panitsidis