Correction: A previous version of this graphic mistakenly identified the missile fired as being the 3M14E – an export version of the submarine-launched missile, rather than the 3M14T – the domestic surface-vessel vertically launched missile.

RUSSIAN CRUISE MISSILE
ATTACK ROUTES INTO SYRIA
RUSSIA
Caspian
Sea
Black
Sea
GEORGIA
AZER.
ARMENIA
TURKEY
AZER.
SYRIA
IRAN
LEB.
Baghdad
Damascus
IRAQ
SAUDI
ARABIA
JOR.
0
300
MILES

RUSSIAN CRUISE MISSILE ATTACK ROUTES INTO SYRIA
KAZAKHSTAN
UKRAINE
MOLDOVA
RUSSIA
ROM.
Crimea
BULG.
GEORGIA
Istanbul
Bosporus
Strait
AZER.
ARMENIA
Ankara
TURKEY
0
300
AZER.
MILES
Tehran
Paths of cruise
missiles
CYPRUS
SYRIA
LEB.
Baghdad
Damascus
IRAN
IRAQ
ISRAEL
JOR.
Cairo
Persian
Gulf
SAUDI
ARABIA
EGYPT
Missile path source: Oct. 7, Russian military video

RUSSIAN CRUISE MISSILE ATTACK ROUTES INTO SYRIA
TERRAIN HEIGHT
TURKEY
0
100
Lake
Urmia
Mediterranean
Sea
MILES
Aleppo
13,100 ft.
11,500
Idlib
Dahuk
LAUNCH
Latakia
9,800
Raqqa
Mosul
8,200
Hama
Irbil
Caspian
Sea
6,600
Homs
Deir al-Zour
4,900
SYRIA
LEBANON
Kirkuk
3,300
IRAQ
IRAN
Beirut
2,650
Lake
Thartha
Damascus
2,000
1,300
Tehran
Samarra
650
0

THE LAUNCH
The 3M14T missiles were launched from the flagship of the strike group, the Dagestan, and from three smaller missile ships.
THE DAGESTAN
Length: 335 feet
Crew: 103
THE GRAD SVIYAZHSK, THE UGLICH
& THE VELIKY USTYUG
Length: 243 feet
Crew: 36
THE LAUNCH BOOSTER
A booster propels the 3M14T missile from its launch capsule to its cruise speed at a height of approximately 500 feet. The booster is jettisoned.
Pop-out
wing
slot
Control
fins
Turbojet
engine
Booster
Stabilizer
Stabilizer
The first liquid-fuel booster stage is fitted with four small lattice stabilizers. The missile can be launched from either a ship or a submarine.
THE LAUNCH
Flight wings pop out of the missile's midsection
Control fins mounted around the jet exhaust
Spent
booster
falls away
The 820-pound booster falls back to earth when the missile’s solid-fuel turbojet engine takes over.
THE MISSILE
The standard 3M14T is a land-attack cruise missile and is reported to be armed with an 882-pound payload.
Engine
intake
Pop-out
wing
Missile length
20 feet, 4 inches
Launch tube diameter
2 feet
Missile weight
2,588 pounds
Range
Over 917 miles
Altitude over sea
66 feet
Altitude over ground
164 feet
Sea level speed
656 - 886 feet/sec
EXPLOSIVE POWER
The missile warhead is filled with a penetrating blast/fragmentation high explosive, with a delayed action fuse.
The turbojet engine is fed air through an intake in the underside
Fuel
Payload
Guidance
systems
MISSILE IN FLIGHT
The subsonic missile is powered by a turbojet engine. Over water, the missile flies as low as 66 feet. The missile is thought to have a cruising speed of between 656 and 886 feet per second at sea level, and a range in excess of 917 nautical miles.
For most of the flight, the missile flies autonomously, following preprogrammed waypoints that permit the missile to fly around known threats, such as air defenses, radar and obstacles. The missiles’ route can be updated mid-course using satellite communication.
A Terrain Contour Matching Enroute (TERCOM) system samples terrain height and then correlates the elevation profile against stored elevation data. Over land, the missile flies as low as 164 feet using TERCOM. Its low altitude makes it a difficult target for enemy air defenses.
The missile is also guided with the Russian equivalent to GPS (GLONASS) for the fight prior to the terminal phase, which guides the missile to a preprogrammed set of coordinates.
The terminal phase to the target either continues to use GLONASS or uses an active radar seeker in the nose.

THE LAUNCH
THE MISSILE
Missile length
20 feet, 4 inches
A booster propels the 3M14T missile from its launch capsule to its cruise speed at a height of approximately 500 feet. The booster is jettisoned.
Launch tube diameter
2 feet
Missile weight
2,588 pounds
Range
Over 907 miles
Altitude over sea
64 feet
Altitude over ground
164 feet
Flight wings pop out of the missile's midsection
Sea level speed
656 - 886 feet/sec
Control fins mounted around the jet exhaust
Engine
intake
Pop-out
wing
Spent
booster
falls away
The standard 3M14T is a land-attack cruise missile and is reported to be armed with an 882-pound payload.
The 820-pound booster falls back to earth when the missile’s solid-fuel turbojet engine takes over.
THE LAUNCH BOOSTER
TARGETING
Control fins
The turbojet engine is fed air through an intake in the underside
Pop-out
wing
slot
Fuel
Turbojet
engine
Pop-out wing
Control
fins
Payload
Booster
Guidance
systems
Stabilizers
The first liquid-fuel booster stage is fitted with four small lattice stabilizers. The missile can be launched from either a ship or a submarine.
The missile warhead is filled with a penetrating blast/fragmentation high explosive, with a delayed action fuse.
MISSILE IN FLIGHT
The subsonic missile is powered by a turbojet engine. Over water, the missile flies as low as 66 feet. The missile is thought to have a cruising speed of between 656 and 886 feet per second at sea level, and a range in excess of 917 nautical miles.
For most of the flight, the missile flies autonomously, following preprogrammed waypoints that permit the missile to fly around known threats, such as air defenses, radar and obstacles. The missiles’ route can be updated mid-course using satellite communication.
A Terrain Contour Matching Enroute (TERCOM) system samples terrain height and then correlates the elevation profile against stored elevation data. Over land, the missile flies as low as 164 feet using TERCOM. Its low altitude makes it a difficult target for enemy air defenses.
The missile is also guided with the Russian equivalent to GPS (GLONASS) for the fight prior to the terminal phase, which guides the missile to a preprogrammed set of coordinates.
The terminal phase to the target either continues to use GLONASS or uses an active radar seeker in the nose.

THE LAUNCH
THE MISSILE
A booster propels the 3M14T missile from its launch capsule to its cruise speed at a height of approximately 500 feet. The booster is jettisoned.
Missile length
20 feet, 4 inches
Launch tube diameter
2 feet
Missile weight
2,588 pounds
Range
Over 917 miles
Altitude over sea
66 feet
Altitude over ground
164 feet
Sea level speed
656 - 886 feet/sec
PATH TO DESTRUCTION
Flight wings pop out of the missile's midsection
The subsonic missile is powered by a turbojet engine. Over water, the missile flies as low as 66 feet. The missile is thought to have a cruising speed of between 656 and 886 feet per second at sea level, and a range in excess of 917 nautical miles.
Engine
intake
Control fins mounted around the jet exhaust
Pop-out
wing
Spent
booster
falls away
For most of the flight, the missile flies autonomously, following preprogrammed waypoints that permit the missile to fly around known threats, such as air defenses, radar and obstacles. The missiles’ route can be updated mid-course using satellite communication.
The standard 3M14T is a land-attack cruise missile and is reported to be armed with an 882-pound payload.
The 820-pound booster falls back to earth when the missile’s solid-fuel turbojet engine takes over.
Control
fins
The turbojet engine is fed air through an intake in the underside
A Terrain Contour Matching Enroute (TERCOM) system samples terrain height and then correlates the elevation profile against stored elevation data. Over land, the missile flies as low as 164 feet using TERCOM. Its low altitude makes it a difficult target for enemy air defenses.
Pop-out
wing
slot
Turbojet
engine
Fuel
Pop-out wing
Control
fins
Payload
The missile is also guided with the Russian equivalent to GPS (GLONASS) for the fight prior to the terminal phase, which guides the missile to a preprogrammed set of coordinates.
Booster
Guidance
systems
Stabilizers
The missile warhead is filled with a penetrating blast/
fragmentation high explosive, with a delayed action fuse.
The first liquid-fuel booster stage is fitted with four small lattice stabilizers. The missile can be launched from either a ship or a submarine.
The terminal phase to the target either continues to use GLONASS or uses an active radar seeker in the nose.
Source: IHS Aerospace, Defence & Security
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