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Weapons of Mass Destruction (WMD)


Mobile ICBMs

Mobile ICBMs Compared

Mobile ICBM Trucks

Rail Mobile ICBMs


KB missile system BR Self-propelled launcher Flight test Year adopted into service notes
KBM (Kolomna) "Gnome" - - Mobile project, 1958-60. 3-speed, 1-st. - 4-nozzle accelerator (SRM, 1.75 m) + solid fuel ramjet (5.5 M), 2nd and 3rd - SRM. Range p. -11000 km, Start. Weight BR - 29-31,2 tons, MS - 0.47 tons, Kazakhstan - 65 tons BR Length. -16.14 m. Work stopped in 1965.
OKB-1 RT-2 (8K98) - - Option w / d based (4 PU on BZHRK) project (beg. Of 1960s)
OKB-586 15P699 (15P099) RT-20P (8K99) 15U21
(SM-SP21)
1967 - Start of development - 1964. On crawler "object 821" rocket launch from TPK using PAD. With a one-piece heavy (1.5 Mt) MS. Level 1 - 4-nozzle (rotating) SRM 15D15 (KBM) thrust of 60 tons, 2nd (8K94) - RD-857 (15D12 or 15D512, AT and UDMH) traction 14-15 m Start.. BR weight - 30,0-30,2 t, MS - 1.41 m length. -17.48 mDiameter - 1.6 m. Range page -. 5000, or7000 km. SU - with inertial gyroscopic devices. CWE - 2-4 km
15P699 (15P099) RT-20P (8K99) 15U21 (SM-SP21) - With a one-piece light (0.55 Mt) MS. Start. Weight - 3030.2 m, MS - 0.545 m length. - 17.8 m. Range p. -11000 km. Weight SPU with BR - approx. 65 m. The work stopped in1969.
OKB-586 RT-21 (15ZH41) SM-SP25 - - Project, 1963. Solid, 3-speed. Weight rockets - 36 m (with TPK - 42 m). TPK Length -17.0 mDiameter - 2.0 m. 6 PU on BZHRK, rockets launched from TPK using PAD
RT-21 (15ZH41) - - Underground, earth-covered igloo, project
RT-21 (15ZH41) SM-SP22,
SP24-SM,
SM-SP26,
SP27-SM,
SM-SP30
- - Silo (MSE "OS" type). Project 1963-66 g.
KB Yuzhnoye RT-22 (15ZH43) SM-SP35 - - BZHRK project 1969. 3-stage solid-BR. The launch of the TPK using PAD. Weight BR - 70 m, with TPK -. 80 m length TPK -18.885 m Diameter - 2.5 m. Range p. -11000 km. 1st Art. - SRM 15D122
MIT
(p/n 2227, Moscow)
"Temp-C2M" - - Project, 1965. 3-stage solid-BR crawler various options. Start. BR weight - 37.0 tons Length -. 1819 m (TPK - 20m) Diameter - 1.8M (TPK - 2m). Range page -. Bol.8000 km. The guidance system - inertial to the GPS (TSNIIAG / NIIAP)
"Uranus" 15ZH42 - - At 6-axle chassis MAZ-547A, 1968.
"Temp-2C" 15ZH42 15U67 - - Project, 1970. On the crawler T-10 ( "object 825 ch. 2") or the T-80 ( "object 825 sp.3")
"Temp-2C" 15ZH42 (PC-14) 15U68 1972 1976 At 6-axle chassis MAZ-7310 (MAZ-547A). With a one-piece MS (Mt 0,65-1,5). Range p. -10500 km. Start. BR weight - 41,5-44,2 t, MS - 0.94 m length. -18.5 mDiameter - 1.79 m. SU - inertial with onboard computer (NIIAP). CWE - 0,45-1.64 km. Weight SPU with BR - approx. 82 tons
"Temp-2SM1" 15ZH47 - - With HSR (3 BB), the project (beginning of the development - 1975).. Range p. -10,000 km
"Temp-2SM2" 15ZH48 - - With HSR (3 BB) project. With more powerful BB Range page. -10500 km. 3rd Art. - 15D68M with rotary nozzle
KB Yuzhnoye 15P952 (15P252) RT-23 (15ZH52) CM-SP-35 1984 - Start of development - 1979. 6 PU on BZHRK experienced. The launch - "mortar" of TPK. MIRV (10h0,3-0,55 Mt) with solid-control BB breeding. 1st Art. - 15D206, 2nd item. - 15D207, 3rd st. - 15D291. Start. weight - 104 tons, MS - 4.05 m .Dlina -. 23,4-23.8 mDiameter - 2.4 m. Range page -. 10000-11000 km. Adopted in trial operation 1983.
15P961 PT 23UTTH (15ZH61) 1985 - Start of development - 1983. Experiental tests. 1st Art. - 15D289, 2nd item. - 15D290, 3rd st. 15D291. Conducted two test launches (2nd - emergency)
15P961 (15P261)
"Well done"
PT 23UTTH
(15ZH61, PC-22A)
15P761 1985 1989 3 PU on BZHRK, rocket launch - "mortar" from TPK using PAD. With MIRV 10h0,43 Mt (15F143 with 4-chamber LRE 15D264). 1st Art. - 15D206, 2nd item. - 15D339, 3rd st. - 15D291. Start. Weight - 104.5 m, MS - 4.05 m length. -22.6 mDiameter - 2.4 m. Range p. -10100 km. SU - with inertial ODCC (AP NGOs). With a folding fairing warhead and recessed nozzles Stage 1 restrictions on the size w / a car. Series in 1987-91 gg., Made 12 BZHRK
KB Arsenal F-22 - - Research "Swirl", 1976-77. IDB on-road train container truck (tractor MAZ-6422 and MAZ-9389 trailer with a unified container UUK-3). Weight BR - 13.5 m length. -11.4 mDiameter - 1.28 m
MIT PT 23UTTH - - The underground mobile RK. Project beginning. 80s. RT-23 Option OKB "South" with the rotary control nozzles SRM 1st and 2nd stages, the increased weight of the fuel, solid-control breeding warheads
PT 23UTTH (15ZH62) - - Project, 1983.
KB Yuzhnoye "Celina-2" (15P962) RT-23 (15ZH62) - - PGRK 6-axle MAZ-7904 or 8-axle chassis MAZ-7906. Start of development -1983.
"Celina-2" RT-23 - - On the 12-axle chassis MAZ-7907, early. 80s., Is not implemented
MIT 15P158 "Poplar" RT-2PM (15ZH58) 15U168 1983 - The mobile missile system. Start of development -1976. 3-stage solid-BR 7-axle chassis MAZ-7917. Fuel - based synthetic rubber in a mixture with a powdered substance and an oxidizing agent - ammonium perchlorate ( "Union" NPO)
15P158 "Poplar"
(RS-12M)
RT-2PM (15ZH58) 15U168 1988 With a one-piece MS (0.55 Mt, VNIIEF) with 4 CT control (similar to RK "Pioneer"), rockets launched from TPK using PAD. Start. BR weight - 46 tons, warhead - 1 m length. -21.5 mDiameter - 1.8M. Range p. -10,000 km. SU - inertial with onboard computer (AP NGOs). CWE -0.9 km. Weight SPU with BR - approx. 98 tons
15P658 "Topol-T" RT-2PM (15ZH58) 15U128 SPU on the MAZ-7912-01 (with a shower ahead)
RT-2PM 1983 - With BG 3-4 (MIRV), experienced
MIT "Topol M"
( "Topol-M2")
PT 2PM2 (RT-2UTTH, 15ZH65) 15U175 2000 - Start of development - 1991. "Unified" 3-stage solid-BR 8-axle chassis MZKT-79221
15P165 "Topol-M"
( "Topol-M2")
PT 2PM2
(RT-2UTTH, 15ZH65)
15U175 2005 The launch of the TPK using PAD. With a one-piece MS (0.55 Mt, VNIIEF), without lattice stabilizers. Start. weight - 47.2 tons, warhead - 1,179 m length. -22.7 mDiameter - 1,86-1.95 m. Range p. -10,000 km. SU - inertial with onboard computer (AP NGOs). CWE -0.35 km
"Topol M" PT 2PM2 15U175 2005 With the maneuvering warhead type MARV
MIT 15P159 "Courier"
(RCC-40)
15ZH59 1992 (plan) - RK Mobile with compact MBR (15 m, similar to the American ICBM "Midzhitmen") on van chassis. Start of development -1981. Type the start - from TPK due to PAD. Start. BR weight - approx. 15 t SU -. Inertial with onboard computer. Work stopped in1991.
MIT "Yars" ( "Yarts") RS-24 2007 - Mobile RK chassis PGRK "Topol" with a prototype 3-stage solid-propellant ICBMs based RT-2PM2 with multiply-charged warhead (3 and 4 BB decoys) 2003. Experiental tests
RS-24 2010 Battle of the RK

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Page last modified: 09-07-2018 13:12:03 ZULU