Missile Dongfeng DF-31 (CH-SS-10)

Summary

NATO DesignationCH-SS-10
CategoryBallistic Missiles
Sub-typeIntercontinental Ballistic Missile
Origin country 🇨🇳 China
ManufacturerAcademy of Rocket Motors Technology
StatusIn service
Year of service2017

Technical specifications

WarheadNuclear MIRV
Diameter2,370 mm (93.3 in)
Length21,600 mm (850.4 in)
Flight altitude1,200,000 m (3,937,008 ft)
Weight54,000 kg (119,049 lb)
Range 11,200 km (6,959 mi)
Max. speed29,376 km/h (Mach 29.4)

Operators

🇨🇳 China

Description

Development of the DF-31 intercontinental ballistic missile began in January 1985. The system was designed as a land-based variant of the JL-2 submarine-launched ballistic missile and was initially designated DF-23. The missile was first displayed publicly at the 1999 National Day Parade. A successful test flight was reported in August 1999, with subsequent test flights conducted in 2000.

The DF-31 is a three-stage, solid-fuel rocket. Guidance is provided by an astro-inertial system utilizing the BeiDou Navigation Satellite System. The baseline missile carries a single one-megaton thermonuclear warhead. The DF-31A variant is designed with multiple independent reentry vehicle (MIRV) capability to carry three to five 90-kiloton warheads, though it may also be configured with a single warhead and penetration aids. This variant also utilizes maneuverable reentry vehicles. The DF-31AG and DF-31B variants provide MIRV capability and utilize an eight-axle off-road transporter erector launcher (TEL). The DF-31BJ is a variant configured for silo-based operations.

The system is operated by the People's Liberation Army Rocket Force in China. The DF-31 entered service in 2006, the DF-31A in 2007, and the DF-31B in 2017. The missile is operationally deployed in both silo and road-mobile configurations. The DF-31AG was first unveiled during a 2017 military parade. There are no recorded instances of combat use.

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