escobar
Brigadier
The DF-3 is China’s first operational intermediate-range ballistic missile. The missile is a single-stage, liquid-propellant design carrying a single nuclear warhead.The DongFeng-3 (DF-3, NATO designation: CSS-2) is a single-warhead, single-stage, liquid-propellant, intermediate-range ballistic missile (IRBM). Developed in the 1960, it is China's first independently developed ballistic missile. The DF-3A is the improved variant with extended range developed in the early 1980s. A total of 150~200 DF-3/3A missiles are believed to have been deployed, with 30~40 remaining in service today.
DongFeng-3 specifications:
Configuration: Single stage liquid
Length: 21.2m
Diameter: 2.25m
Launch Weight: 64,000kg
Propellant: Liquid fuel (Unsymmetrical Dimethylhydrazine/Nitrogen Tetroxide mix [UDMH/N2H4])
Guidance: Inertial
Range: 2,500km (DF-3); 2,800km (DF-3A)
Deployment: Launch pad + road mobile
Re-entry Vehicle Mass: 2,150kg
Warhead: Single 1,000~3,000kT
CEP: 2,000~3,000m (DF-3); 1,000m (DF-3A)
Launch Preparation Time: 120~180 min
The DongFeng 4 (NATO reporting name: CSS-3) liquid-propellant, two-stage intermediate-range ballistic missile (IRBM) was developed by the China Academy of Launch Vehicle Technology (CALT, also known as 1st Space Academy) in the 1960s. The missile entered operational service in the early 1980s, with approximately 20 missiles (2008 Pentagon report) currently deployed by the PLA Second Artillery Corps. The DongFeng 4 was also used to develop PRC’s first space launch vehicle Changzheng 1 (Long March 1), which sent the country’s first satellite into the orbit in 1970.
DongFeng-4 specifications:
Official name: DongFeng 4 (DF-4)
NATO reporting name: CSS-3
Contractor: China Academy of Launch Vehicle Technology (CALT)
Service status: In service
Configuration: Two-stage, liquid propellant
Deployment: Silo and semi-mobile (towed trailer)
Propellant: Unsymmetrical Dimethylhydrazine/Nitrogen Tetroxide mix (UDMH/N2H4)
Length: 28m
Diameter: 2.25m
Launch weight: 82,000kg
Range: 4,750km
Re-entry vehicle mass: 2,200kg
Warhead: Single, 1,000~3,000kT yield thermalnuclear
Guidance: Inertial
Accuracy: CEP 1,500m
Launch preparation time: 3~5 hours (mobile), or 2~3 hours (silo)