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SOV - 8K63 / R-12 / SS-4 Sandal :: USSR / Successional Countries USSR (RUS/SOV) :: Strategic Missile Systems (range more than 1000 km)

Display link [ Funkce ]  [ Snakeavatar ]
R-12, 8K63, R-12, SS-4 Sandal
R-12U 8K63U, R-12, SS-4 Sandal
Basic information

Start of development:
R-12-13 August 1955
R-12U - 30 May 1960
Design office: OKB-586
Manufacturer: Race 586, Dnepropetrovsk, Omsk air factory
Flight tests:
R-12 - June 22, 1957 - December 1958
R-12U - December 1961 - December 1962
Combat Duty: 15 May 1960 (open position), January 1, 1963 (Silo)
Entry into service:
R-12-4 March 1959
R-12U - 9 January 1964
Number of stages: 1
Drive: shelf stable liquid fuel
Launchers:
R-12 - land open
R-12U - open land, launchers Dvina (hot fire)
The number of heads and power: 1x2.3 Mt
The combat load: 1.6 t
Maximum range: 2080 km
Seeker: inertial Home
Accuracy: The maximum error of 5 km
Length: 22.1 m
Maximum diameter: 1.65 m
Starting weight: 47.1 t
Fuel Weight: 37.0 t
Oxidant: AK-27I (27% mixture of nitrogen tetroxide and nitric acid 73% inhibited by iodine)
Fuel: kerosene TM-185
Thrust (sea level / vacuum): 628 / 721 kN
Specific impulse (sea level / vacuum): 2237 / 2570 m / s
Preparing the shot: 205 minutes, from the state of preparedness of 4, 140 minutes, from the state of preparedness of three, 60 minutes from the state of preparedness of 2, 30 minutes from a state of readiness
Life: 7 years in a state of readiness of 4 and 3 years in a state of preparedness of 3, three months in a state of readiness 2, 30 days in a state of readiness

Source: Russian Strategic Nuclear Forces, Pavel Podvig, Oleg Bukharin, MIT Press, Cambridge, 2001
(Original: Raketnije troops strategičeskogo naznačenija)
SOV - 8K63 / R-12 / SS-4 SandalDisplay link [ Funkce ]  [ Martin Smíšekavatar ]
...
R-12 (3).jpg

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(FAS.org)
R-12 (2).jpg

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(FAS.org)
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(FAS.org)
ustanovščikDisplay link [ Funkce ]  [ Jiri Kouba ]
I would really like to know from where he took a piece of art if it was the basis for a construction machine, or is it just a device developed for military purposes. According to the available shots lifted the arm 180 degrees, put his racket on the container, returned to the starting position, poodjelo odpalovacímu the table, rose up and ordered the rocket upright on her table. Then the rocket ukolmila, fix the before launching the arm disconnected and returned to the starting position, the rocket remained in standby mode on the table.
ustanovščik v praxiDisplay link [ Funkce ]  [ Jiri Kouba ]
establishment under kapyar.km.ru looked like rockets. It is worth noting container, which creates
left side of the towers for the establishment and training. On the right you can see the back of ustanovšik-A.
r12_3.jpg

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odpovím si sámDisplay link [ Funkce ]  [ Jiri Kouba ]
So this is called ustanovščik 8U224 (8U224M) and is built on the basis of uniaxial truck MAZ-529, later MoaZ-546, the civilian use skejpru. Each modification to label ustanovščiku 8U210, 8U224, 8U224P, 8U224М.
They were used as bedrooms above-ground release for R-14 (SS-5), R-16 (SS-6) and R-36 (SS-9).
SS-4 v pochodovém prouduDisplay link [ Funkce ]  [ Jiri Kouba ]
Raketu runs the conveyor Artillery Tractor AT-T.
r-12-full.jpg

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karibská krizeDisplay link [ Funkce ]  [ Jiri Kouba ]
the fall of 1962 located 36 missiles fired from land-mobile launcher
(Ustanovka - firing table) ustanovščik + (transporter-erector) Cuba near the town of San Cristobal in Operation Anadyr.
Display linkAdmin 21.09.2008 09:45:07 [ Funkce ]  [ buko1avatar ]
By missile system kit included the following elements:

8U217 (8У217) - launchers (blasting table), weight 6.9 tons, dimensions 3020x3020x3270 mm
8U210 (8У210) - Charging Transport missiles based jednooséh oťahača MAZ-529V (МАЗ-529В), or MoAZ-546 (МоАЗ-546) (JaAZ-206 engine with performance 165/215 hp, Dimensions (LxWxH) 15620x3150x3176 mm)
8T115 (8Т115) - missile transporter chassis with a container with the tractor MAZ-535 (МАЗ-535), or MAZ-529 (МАЗ-529) or AT-T (АТ-Т) 22580x2720x2500 dimensions mm
8G112 (8Г112) - fuel tank on the chassis triax
8G113 (8Г113) - Refueling oxidant
8G131 (8Г131) - oxidizer tank
8G210 (8Г210) - heater-filler hydrogen peroxide-based ZIL-157 (ЗИЛ-157)
8G11 (8Г11) - tank of hydrogen peroxide-based ZiS-151 (ЗиС-151)
8T555 (8Т555) - Transportation oxidizer tank (10700x2630x3350 mm)
?? - Transportation fuel tank (11380x2630x2960 ​​mm)
8T318 (8Т318) - vehicle cable joints
8N112 (8Н112) - test vehicle
8N113 (8Н113) - test vehicle (horizontal test)
8N213 (8Н213) - a vehicle for training (box body (КУНГ) chassis ZIL-157 (ЗИЛ-157)
8N214 (8Н214) - generator
8N215 (8Н215) - No cable car. 1 (van body ZIL-157 )
8N216 (8Н216) - No cable car. 2 (van body ZIL-157 )
8N217 (8Н217) - vehicle heating head
8N218 (8Н218) - the cable car technical position?
8T310 (8Т310) - vehicle accessories, with technical positions
8T331 (8Т331) - ZIP department for electrical discharge (van body ZIL-157 )
8G27 (8Г27) - gasoline-electric air heater
8G33 (8Г33) - air compressor based ZiS-151 (ЗиС-151)
8T325 (8Т325) - No vehicle with ZIP. 1 (engine compartment)
8T330 (8Т330) - No vehicle with ZIP. 2 (starter gear)
8T216 (8Т116) - automatic height
8Š14 (8Ш14) - a set of guidance tools
8Š31 (8Ш31) / DDN-1 (ДДН-1) - photoelectric moisture indicator
8Ju12 (8Ю12) - tent technical positions (served in protection rackets, length 30 m, width 5 m, construction of pipe hlíkových)
8T311 (8Т311) - car washing and neutralizing
8T26 (8Т26) - automobiloý crane 10 t
ESD-20-VS/400 (ЭСД-20-ВС/400) - diesel generator (20 kW, 3 x 400 V/50 Hz) biaxial trailer for 2-PN-2 (2-ПН-2)
ESD-50-VS/400 (ЭСД-50-ВС/400) - diesel generator (50 kW, 3 x 400 V/50 Hz) biaxial trailer for 2-PN-4 (2-ПН-4)
?? - Radio control car jump
8F12N (8Ф12Н) - head rackets
?? - Ground equipment for maintenance head
?? - Vehicle storage head
8N122 (8Н122)
8N231 (8Н231)
8N65 (8Н65)
8N66 (8Н66)
8N67 (8Н67)

Source: http://ruzhany.narod.ru/rvsn/SS_4.html
Display linkAdmin 21.09.2008 10:13:05 [ Funkce ]  [ buko1avatar ]
Preparation time rockets firing:
- 3 to 3.5 hours (rocket in technical positions, without fuel, gyros, and head)
- 2.3 hours (in the technical position of the rocket, equipped with gyroscopes and warhead)
- 1 hour (the rocket is in the firing position, no fuel)
- 30 min (the rocket is firing position, filled with fuel)
- 5 min (missile in firing position, and after refueling predštartovej preparation, without starter codes)

Rocket Division 8K63/8K63U be armed in his report, usually 5 missile regiments. Rocket Regiment was formed:
- Option 1: 2 x rocket section with complex 8P863 (8П863), each complex was formed packs four batteries, each battery should have 2 rockets. Total of 16 missiles ready to launch.
- Option 2: 2 x rocket section with complex 8P863 (8П863), each complex consists of two batteries, each battery 2 missiles, 1 x rocket section with complex 8P763 (8П763) and four launcher - a total of 8 launcher, 4 rockets depots, conveyors 11-14, 6-7 charging conveyors, 45-52 tanks of fuel.
- Option 3: 2-3 x rocket section with their start complex 8P763 (8П763), a total of 8-12 launcher (16-24 missiles).

The firing positions were depots and missile firing position located approximately 175 m.

NB.: Due to frequent changes in the structure raketovýh troops is likely that there are other variants of the structure of individual regiments.

Source: http://ruzhany.narod.ru/rvsn/SS_4.html
Display linkAdmin 21.09.2008 10:45:50 [ Funkce ]  [ buko1avatar ]
Loading missiles on a charging system 8K63U Transport 8U210 by crane 8T26 .

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