1.Name: Trident II (D5)
   Manufacturer: USA
   Produced: 1977—1990
   Entered service: 1990

   Length: 13,42 m
   Diameter: 2,11 m
   Maximum firing range: 11 000 km
   Propulsion: Three-stage solid propellant
   Launch Weight: 59 078 kg
   Throw weight: 2800 kg
   Types of Warhead: Nuclear MIRV (Multiple Independently Targetable Reentry Vehicles)
   Circular probable deviation: 120 m
   Guidance system: Astro-inertial with GPS
   Warhead: W76 100 kT or W88 475 kT
   Number of MIRVs: 8 x 475 kT

2.Name: R-36M (SS-18 Satan)
   Manufacturer: Russia
   Produced: 1970
   Entered service: 1988

   Length: 33,65 m
   Diameter: 3 m
   Maximum firing range: 16 000 km
   Propulsion: Two-stage liquid propellant
   Launch Weight: 209 200 kg
   Throw weight: 8800 kg
   Types of Warhead: Nuclear MIRV (Multiple Independently Targetable Reentry Vehicles)
   Circular probable deviation: 430 m
   Guidance system: Inertial, autonomous
   Warhead: 0.8 – 1 MT
   Number of MIRVs: 10

3.Name: RS-24 Yars
   Manufacturer : Russia
   Produced: 2004
   Entered service: 2010

    Length: 23 m
   Diameter: 2 m
   Maximum firing range: 12 000 km
   Propulsion: Three-stage solid propellant
   Launch Weight: 46500-47200 kg
   Throw weight: 1180-1250 kg
   Types of Warhead: Nuclear MIRV (Multiple Independently Targetable Reentry Vehicles)
   Circular probable deviation: 150 m
   Guidance system: Inertial with ‎Glonass
   Warhead: Nuclear, 150-200 kT. Propulsion
   Number of MIRVs: 10

4.Name: LGM-30G Minuteman III
   Manufacturer : USA
   Produced: 1965-1972
   Entered service: 1970

   Length: 18.2 m
   Diameter: 1.85 m
   Maximum firing range: 13000 km
   Propulsion: Three-stage solid propellant
   Launch Weight: 35400 kg
   Throw weight: 10 tons
   Types of Warhead: Nuclear MIRV (Multiple Independently Targetable Reentry Vehicles)
   Circular probable deviation: 0.18-0.28 km
   Guidance system: Minimum Essential Emergency Communications Network, or MEECN. MEECN receives extremely-high frequency and very-low frequency signals coming 

                                   from ground stations
   Warhead: 3x W-62 thermonuclear (170 kT) in 3x Mk.12 MIRV (or 3x W-78 thermonuclear (340 kT) in 3x Mk.12A MIRV)
   Number of MIRVs: 3

5.Name: R-29RMU2.1 Layner
    Manufacturer : Russia
    First launch: 2011
    Entered service: 2014

    Length: 15 m
    Diameter: 1,9 m
    Maximum firing range: 12 000 km
    Propulsion: Three-stage liquid-propellant rocket
    Launch Weight: 40 300 kg
    Throw weight: 2 800 kg
    Types of Warhead: Nuclear MIRV (Multiple Independently Targetable Reentry Vehicles)
    Circular probable deviation: 500 m
    Guidance system: Astro-inertial with GLONASS update
    Warhead: 4 × 500kt or 12 × 100kt multiple thermonuclear warheads
    Number of MIRVs: 4

6.Name: M51
   Manufacturer : France
   Produced: 1990 
   Entered service: 2010

   Length: 12 m
   Diameter: 2.3 m
   Maximum firing range: 10 000 km
   Propulsion: 3 stage solid
   Launch Weight: 52 000 kg
   Throw weight: –
   Types of Warhead: Nuclear MIRV(Multiple Independently Targetable Reentry Vehicles)

                                     with ABM (anti-ballistic missile)
   Circular probable deviation: 250 m
   Guidance system: Astro-inertial guidance. Galileo (satellite navigation)
   Warhead: 6 to 10 TN 75 MIRV 110 kiloton (kt) (420 TJ), with penetration aids
   Number of MIRVs: 6-10 x 107 kT

7.Name: DF-41
   Manufacturer : China
   Produced: The project has been under development since the 1980
   Entered service: 2017

   Length: 19.5 m
   Diameter: 2 m
   Maximum firing range: 12 000 km
   Propulsion: Three-stage Solid-fuel rocket
   Launch Weight: 80 000 kg
   Throw weight: 3000-3200 kg
   Types of Warhead: Nuclear MIRV(Multiple Independently Targetable Reentry Vehicles)
   Circular probable deviation: 150-200 m
  Guidance system: Inertial, likely with stellar updates and BeiDou
  Warhead: Thermonuclear weapon, single 1 Megaton or MIRV with selectable 20, 90, 150 kiloton
  Number of MIRVs: up to 10

8.Name: DF-31AG
   Manufacturer : China
   Produced: 1985
   Entered service: 2006
   Length: 13 m

   Diameter: 2.25 m
   Maximum firing range: 11 700 km
   Propulsion: Three-stage solid propellant
   Launch Weight: 42 000 kg
   Throw weight: –
   Types of Warhead: Nuclear MIRV(Multiple Independently Targetable Reentry Vehicles) and TEL( Transporter Erector Launcher) vehicle is based on 8-axle Taian special 

                                      wheeled chassis
   Circular probable deviation: 500 km
   Guidance system: Astro-inertial guidance with BeiDou Navigation Satellite System
   Warhead: Nuclear 1-3 MT
   Number of MIRVs: 10

9.Name: JL-2
   Manufacturer : China
   Produced: 1990
   Entered service: 2004

   Length: 13 m
   Diameter: 2m
   Maximum firing range: 7200 km
   Propulsion: Three-stage solid propellant
   Launch Weight: 42 000 kg
   Throw weight: –
   Types of Warhead: –
   Circular probable deviation: 200 m
  Guidance system: Astro-inertial with Beidou
   Warhead: Nuclear 250-1000 kT
   Number of MIRVs: 3 or 4

10.Name: Bulava
     Manufacturer : Russia
     Produced: 1998
     Entered service: 2018

     Length: 12.1 m
     Diameter: 2 m
     Maximum firing range: 8000-9300 km
     Propulsion: 3-stage solid-fuel
     Launch Weight: 36 800 kg
     Throw weight: 1150 kg
     Types of Warhead: Nuclear MIRV(Multiple Independently Targetable Reentry Vehicles)
    Circular probable deviation: 350 m
    Guidance system: Astro-inertial guidance with On-board digital computer complex
    Warhead: Nuclear triad 150 kT
    Number of MIRVs: 6-10