In numbers Through the lens Video
976 SKIP Command test center aircraft (Monitoring and recording of nuclear explosions and missile launches).
Aircraft command and measurement point based on the Il-76MD with the "Shmel" RTK (a rotating RF-2 module with a diameter of about 11 m and a height of 1.5 m) and four D-30KP turbofan engines with a thrust of 12.000 kgf each.
Aircraft command and measurement point based on the Il-76MD with the "Shmel" complex (a rotating RF-2 module with a diameter of about 11 m and a height of 1.5 m) and four D-30KP turbofan engines with a thrust of 12.000 kgf each. The first flight took place in 1986. A total of 5 units were produced, of which 3 were decommissioned.
The "Shmel" signals intelligence complex has a tracking range of objects and ranges from 400 km for low-altitude objects and up to 2-3 thousand km for high-flying ones, and with group use of the "SKIP" - more than 10.000 km.
Technical specifications
| DESIGNER | OKB Ilyushin, Beriev |
| COUNTRY | Russia |
| TYPE |
Monitoring and recording of nuclear explosions and missile launches
|
| CREW | 5 |
| POWER-PLANT | Four turbofan engines D-30KP |
| Thrust, kgf | 4x12.000 |
| DIMENSIONS | |
| Length, m | 46,59 |
| Height, m | 14,80 |
| Wing span, m | 50,50 |
| Wing area, m2 | 300,00 |
| Diametr antenna, m | 10,20 |
| WEIGHT | |
| Maximum take-off, kg | 190.000 |
| Normal take-off, kg | 180.000 |
| Empty aircraft, kg | - |
| Internal fuel, kg | - |
| Payload, kg | - |
| PERFORMANCE | |
| Maximum speed, km/h | 780 |
| Economic speed, km/h | - |
| Cruising speed, km/h | - |
| Service ceiling, m | 12.000 |
| Range without aerial refueling, km | 6.800 |
| Combat range, km | - |
| ARMAMENT | Doesn't have (defensive). |