The Izdelie-30 cruise missile
Front fuel tank
View
Side fuel tanks
View
Warhead
Manufacturer: GOSNIIMASH JSC
View
Fuel dosing unit
View
Pyrovalve of the pneumatic system
View
Pyropatron DP4-3M
Manufacturer: MPZ JSC
View
GNSS receiver with digital antenna array "Kometa-M12"
Manufacturer: VNIIR-PROGRESS JSC
View
Receiving and computing unit (RCU) with NAVIS NR9 satellite signal receiver
Manufacturer: KB NAVIS JSC
View
Pyropatron DP4-3M
Manufacturer: MPZ JSC
View
Pneumatic cylinder for wing folding system
View
Wing consoles
View
Turbojet twin-circuit engine "Izdeliye 64R"
Manufacturer: ODK-SATURN PJSC
View
Target contact sensors
View
Chemical power source UB-BS of the warhead initiation system
Manufacturer: PEMZ MOLOT JSC
View
BUBS-30 warhead equipment control unit
Manufacturer: ZIP PJSC
View
Nitrogen pneumatic units
View
Boost pressure reducer
View
BS-M84G426 coupling block
Manufacturer: ANPP TEMP AVIA JSC
View
Suspension device for an aircraft carrier's aviation catapult device
View
Electrical connector locking mechanism
View
Specifications
| Wingspan | 3 m |
| Housing diameter | 580 mm |
| Range | at least 1,500 km |
| Speed | 720 km/h |
| Weight of the warhead | 800 kg |
| Flight altitude | 200 - 2000 m |
Total: 24
