S-300PM (S-300PMU-1), NATO code SA-20A Gargoyle antiaircraft missile system, modernization of the system development on the basis of the PLRK S-300P began in 1985, introduced into the armament of the air defense of the Russian Federation in 1993. Released for export under the designation S-300PMU-1.
The main difference between the S-300PM and previous tristovkas is the use of the new 48N6 missile (and its export variant 48N6E) developed by the NPO "Fakel" design bureau. The missile is capable of destroying air targets flying at speeds of up to 6,450 km/h, at a range of 150 km. It is capable of destroying low-flying cruise missiles at altitudes of 6-100 m at a range of 35-38 km. The system includes a sophisticated antenna system of target irradiation radar and missile guidance. The system is available in a mobile variant on MAZ chassis, as well as in a variant on tractor-trailers pulled by KrAZ tractors (the different parts are compatible with each other). The S-300PM is part of Moscow's S-50 air defense system.
Composition of the S-300PM and S-300PMU-1:
- anti-aircraft cruise missile, 48N6 (48Н6), 48N6E (48Н6Е), or 48N6E1 (48Н6Е1)
- anti-aircraft missile complex 90Ž6E (90Ж6Е) composed of:
---- multifunction radar target irradiation and missile guidance 30N6E (30Н6Е) :
---- to 12 5P58SE (5П85СЕ) launchers on a car chassis MAZ-547 (МАЗ-547), or 5P85TE (5П85ТЕ) towed by a tractor KrAZ-260 (КрАЗ-260), with four containers with missiles on each (the complex can also work with the older 5P85S launchers, or the trailer-mounted OZ 5P85T (5P85TM, 5P85SM)
---- 1T12M2 (1Т12М2)
---- means of missile transport and maintenance - rechargeable transporter 22T6E (22Т6Е), missile transporter 5T85E (5Т58Е) (or older transporters 5T99, 5T99M)
- hydraulic lifting platform 40V6M(40В6М) for RPN 30N6E (30Н6Е)
- A radar for detecting low-flying targets76N6(76Н6Н6)
- technical security assets
---- power plant 5I57A
---- transformer 82H6 and 83H6
---- other means similar to S-300PS
The fire element of the S-300PM complex, the S-300PMU-1, cooperates with 36D6 surveillance radars or 96L6 automated command system 96L6 in conducting combat operations.cz/viewtopic.php/t/40093]83M6E1[/url], controlled by automated command systems 5S99M "Senezh" (5S99M-1 Senezh-M, 5S99M-2 Senezh-M1E) and 5N37 "Baikal", 73N6 "Baikal-1" (via cabin 53L6)
Tactical-technical data:
Year of entry into service: 1993
PLRS type: 48N6, 48N6E - export (48Н6, 48Н6Е)
Missile guidance sector width in azimuth: 90°
Area of effective range
- Max. range (aerodynamic target): 150 km
- Max. range (ballistic target): 40 km
- min. range: 3-5 km
- Minimum altitude (aerodynamic target): 10 m
- max. altitude (aerodynamic target): 27 km
Max. Rocket speed: 2100 m/s
Max. Target speed: 1800 m/s (2800 m/s for radio-controlled missile guidance)
Number of simultaneously tracked targets: up to 12*
Number of simultaneous targets shot: up to 6
Number of missiles simultaneously guided: up to 12
Min. time between missile launches: 3 s
System deployment/deployment time: up to 5 min / up to 5 min
Missile guidance method: autonomous (48N6)
Number of missiles in the firing element: 32 - 48
*Number of simultaneously tracked targets is given with respect to one firing element (plrbat), the number of simultaneously tracked targets at the plro command post, plrb PVO depends on the automated command system used.
For more information on the S-300P development line, see S-300P.
The main difference between the S-300PM and previous tristovkas is the use of the new 48N6 missile (and its export variant 48N6E) developed by the NPO "Fakel" design bureau. The missile is capable of destroying air targets flying at speeds of up to 6,450 km/h, at a range of 150 km. It is capable of destroying low-flying cruise missiles at altitudes of 6-100 m at a range of 35-38 km. The system includes a sophisticated antenna system of target irradiation radar and missile guidance. The system is available in a mobile variant on MAZ chassis, as well as in a variant on tractor-trailers pulled by KrAZ tractors (the different parts are compatible with each other). The S-300PM is part of Moscow's S-50 air defense system.
Composition of the S-300PM and S-300PMU-1:
- anti-aircraft cruise missile, 48N6 (48Н6), 48N6E (48Н6Е), or 48N6E1 (48Н6Е1)
- anti-aircraft missile complex 90Ž6E (90Ж6Е) composed of:
---- multifunction radar target irradiation and missile guidance 30N6E (30Н6Е) :
---- to 12 5P58SE (5П85СЕ) launchers on a car chassis MAZ-547 (МАЗ-547), or 5P85TE (5П85ТЕ) towed by a tractor KrAZ-260 (КрАЗ-260), with four containers with missiles on each (the complex can also work with the older 5P85S launchers, or the trailer-mounted OZ 5P85T (5P85TM, 5P85SM)
---- 1T12M2 (1Т12М2)
---- means of missile transport and maintenance - rechargeable transporter 22T6E (22Т6Е), missile transporter 5T85E (5Т58Е) (or older transporters 5T99, 5T99M)
- hydraulic lifting platform 40V6M(40В6М) for RPN 30N6E (30Н6Е)
- A radar for detecting low-flying targets76N6(76Н6Н6)
- technical security assets
---- power plant 5I57A
---- transformer 82H6 and 83H6
---- other means similar to S-300PS
The fire element of the S-300PM complex, the S-300PMU-1, cooperates with 36D6 surveillance radars or 96L6 automated command system 96L6 in conducting combat operations.cz/viewtopic.php/t/40093]83M6E1[/url], controlled by automated command systems 5S99M "Senezh" (5S99M-1 Senezh-M, 5S99M-2 Senezh-M1E) and 5N37 "Baikal", 73N6 "Baikal-1" (via cabin 53L6)
Tactical-technical data:
Year of entry into service: 1993
PLRS type: 48N6, 48N6E - export (48Н6, 48Н6Е)
Missile guidance sector width in azimuth: 90°
Area of effective range
- Max. range (aerodynamic target): 150 km
- Max. range (ballistic target): 40 km
- min. range: 3-5 km
- Minimum altitude (aerodynamic target): 10 m
- max. altitude (aerodynamic target): 27 km
Max. Rocket speed: 2100 m/s
Max. Target speed: 1800 m/s (2800 m/s for radio-controlled missile guidance)
Number of simultaneously tracked targets: up to 12*
Number of simultaneous targets shot: up to 6
Number of missiles simultaneously guided: up to 12
Min. time between missile launches: 3 s
System deployment/deployment time: up to 5 min / up to 5 min
Missile guidance method: autonomous (48N6)
Number of missiles in the firing element: 32 - 48
*Number of simultaneously tracked targets is given with respect to one firing element (plrbat), the number of simultaneously tracked targets at the plro command post, plrb PVO depends on the automated command system used.
For more information on the S-300P development line, see S-300P.