In numbers Through the lens Video
NATO reporting name: AS-24 Kiljoy
Αlso known as: Izdeliye 9-A-7660
Entered service: 2017
The hypersonic rocket aviation complex developed on the basis of the 9M723 "Iskander-M" and is designed to effectively destroy ships as aircraft carriers, cruisers, destroyers and the frigate as well as on stationary objects.
The first missiles have been certified for the MiG-31 carrier aircraft and concern the first stage of modernization.
The modified aircraft were of the series:
MiG-31 – prototype (1975), MiG-31 built 1982, of production aircraft, MiG-31 year 1988 with different intake and other structural elements etc, MiG-31D3 built in 1983, equipped with an aerial refueling system, MiG-31B built 1988-1993 and MiG-31M/D built 1986.
The maximum range of the missile with an aircraft-bearer is 2.000 km.
The aircraft that flew the trials with serial numbers were the first modified MiG-31BM: Serial number 592 RSK MiG, “Red 90”, “Red 91”, “Red 92”, “Red 93” and “Red 94”. Second stage concerning the modernization of 113 MiG-31 to MiG-31BM/BMS/K level.
| Kh-47M2 “Kinzhal” Supersonic missile |
 |
| 1 Power Plant: solid-propellan rocket 2 Max speed 12.250 -14.700 km/h 3 Air-launched ballistic missile: it carry both conventional and nuclear warheads. |
Air-launched ballistic missile Kh-47M2 “Kinzhal” (izdelie 9-A-7660)
Three-view drawing
Technical specifications
| DESIGNER | PJSC United Aircraft Corporation (UAC) |
| COUNTRY | Russia |
| TYPE |
Supersonic missile
|
| Aircraft-bearer (aerial means) |
MiG-31BM/BMS/K, Tu-22M3M, Tu-160, Su-57
|
|
POWER-PLANT
|
Solid propellant rocket
|
|
Thrust, kgf
|
- |
|
DIMENSIONS
|
|
|
Length, m
|
7,3 |
| Wing span, m | - |
|
- folded
|
1,6
|
| Fin span, m | - |
| Diameter, m | 0,92 (1,2) |
|
WEIGHT
|
|
|
Maximum missile weight, kg
|
3.800 (4.300) |
|
Weight of solid fuel
|
2.500
|
|
Warhead weight, kg
|
482
|
|
PERFORMANCE
|
|
|
Maximum speed, km/h
|
12.250 - 14.700 |
|
Flight altitude of the missile aircraft-bearer), m
|
15.000 - 25.000 |
|
Maximum range of the missile with a caircraft-bearer, km
|
2.000 |
|
Combat range, km
|
600 |
|
Minimum permissible missile launch range, km
|
- |
|
Permissible speed of the aircraft before using the missile, km/h
|
2.100 - 3.000 |
| Missile velocity when striking with a target, km/h | 4.650 |
|
Circular error probable, m
|
1 |
|
Warhead type
|
High-explosive or nuclear |
|
Guidance system
|
|
|
Combined with:
|
Inertial navigation system (INS) with the possibility of from GLONASS, AWASC, remote control and optical homing system. |