Encyclopedia Astronautica Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9 A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z JL-2 AKA: CSS-N-4; Julang-2. Status: Active. First Launch: 2004-07-01. Last Launch: 2012-08-16. Number: 4 . Payload: 700 kg (1,540 lb). Gross mass: 20,000 kg (44,000 lb). Height: 11.00 m (36.00 ft). Diameter: 2.00 m (6.50 ft). Apogee: 1,000 km (600 mi).
Maximum range: 7,900 km (4,900 mi). Number Standard Warheads: 1. Warhead yield: 250 KT. Boost Propulsion: Solid rocket. Initial Operational Capability: 1998.
Family: ICBM, submarine-launched. Country: China. Launch Sites: Yellow Sea Launch Area. Agency: ARMT. More at: 8348. 2004 July 1 - . Launch Site: Yellow Sea Launch Area. Launch Pad: 35.0 N x 125.0 E. Launch Platform: XIA. LV Family: DF-31. Launch Vehicle: JL-2. FAILURE: Failure. 2005 June 12 - . Launch Site: Yellow Sea Launch Area. Launch Pad: 35.0 N x 125.0 E. Launch Platform: XIA. LV Family: DF-31. Launch Vehicle: JL-2. 2008 May 29 - . Launch Site: Yellow Sea Launch Area. Launch Platform: XIA. LV Family: DF-31. Launch Vehicle: JL-2.
2012 August 16 - . Launch Pad: Xia sub, Bohai. Launch Platform: T094. LV Family: DF-31. Launch Vehicle: JL-2.
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