Artistic illustration Kh-47M2 © Konstantinos Panitsidis
Technical specifications 
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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.
Max operational range (aircraft-bearer) up to 2000 km
The Kh-47M2 missile is transported by modified aircraft: the MiG-31 fighter and interceptor, the Tu-22M3M strategic bomber as well as the fifth generation Su-57 fighter.
Air-launched ballistic missile
1 Power Plant: solid-propellan rocket 2 Max speed 12250 km/h 3 Air-launched ballistic missile: it carry both conventional and nuclear warheads
THREE-VIEW DRAWING
TECHNICAL SPECIFICATIONS
| AIRCRAFT-BEARER | MiG-31BM/BMS/K, Tu22M3M and Su-57 |
| DESIGNER | PJSC United Aircraft Corporation (UAC) |
| Length, m | - |
| Diameter, mm | - |
| Fin span, mm | - |
| Weight, kg | 3.800 |
| Fuel weight (solid-propellan rocket) | 2.500 |
| Warhead type | High-explosive |
| Warhead weight, kg | 482 |
| Guidance system | Inertial navigation system (INS) with the possibility of from GLONASS, AWASC, remote control and optical homing system. |
| Combat range, km | 600 |
| Circle of equal probability, m | 1 |
| Speed, Mach | 10 |
| Rocket velocity when striking with a target, km/h | 4.650 |
| Missile launch speed (aircraft-bearer), km/h | 2100-2400 |
| Flight altitude of the rocket (aircraft-bearer), m | 15000 – 18000 |
