Mobile ICBMs |
Mobile ICBMs ComparedMobile ICBM TrucksRail 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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