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DF-2A
Part of R-12
Chinese intermediate range ballistic missile. Extended-range version of DF-2. The missile featured reduced thrust, but 20% more range, and used autonomous gyroscopic guidance in place of the DF-2's radio system.

AKA: Dong-Feng 2A. Status: Retired 1966. First Launch: 1965-11-01. Last Launch: 1966-10-27. Number: 2 . Payload: 1,500 kg (3,300 lb). Gross mass: 31,900 kg (70,300 lb). Height: 20.61 m (67.61 ft). Diameter: 1.65 m (5.41 ft). Span: 2.13 m (6.98 ft). Apogee: 200 km (120 mi).

Maximum range: 1,250 km (770 mi). Number Standard Warheads: 1. Warhead yield: 20 KT. CEP: 3.71 km (2.30 mi). Boost Propulsion: Storable liquid rocket. Initial Operational Capability: 1970. Total Number Built: 50.



Family: IRBM. Country: China. Launch Sites: Jiuquan, Jiuquan LA3. Stages: DF-2A-1. Agency: CALT.

1964 October 16 - . LV Family: R-12. Launch Vehicle: DF-2A.
1964 November 4 - . LV Family: R-12. Launch Vehicle: DF-2A.
November 1965 - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA3. LV Family: R-12. Launch Vehicle: DF-2A.
1966 October 27 - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA3. LV Family: R-12. Launch Vehicle: DF-2A.

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