Trisha Shetty (Editor)

Long March 2C

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Function
  
Carrier rocket

Height
  
42 metres (138 ft)

Manufacturer
  
CALT

Diameter
  
3.35 metres (11.0 ft)

Country of origin
  
People's Republic of China

Mass
  
233,000 kilograms (514,000 lb)

Long March 2C (LM-2C), or Chang Zheng 2C (CZ-2C) as in Chinese pinyin is a member of the Long March 2 rocket family, an expendable launch system operated by the People's Republic of China. This vehicle was developed by the China Academy of Launch Vehicle Technology, and the first launch occurred on September 9, 1982. It is a two-stage launch vehicle with storable propellants, consisting of Nitrogen Tetroxide and Unsymmetrical Dimethyl Hydrazine. The rocket was derived from the Long March 2A launch vehicle.

Several variants of this launch vehicle have been built, all using an optional third solid motor stage:

  • 2C/SD — Commercial satellite launcher with a multi-satellite smart dispenser allowing delivery of two satellites simultaneously
  • 2C/SM — Version for delivery of small satellites to high orbits
  • 2C/SMA — Improved version of the 2C/SM
  • Shijian 11-04 launch failure

    On August 18, 2011, a Long March 2C rocket failed during the launch of the Shijian 11-04 satellite. During the powered flight phase of the second stage, the connecting mechanism between vernier engine no.3 and the servo-control mechanism of the second stage failed, which led to loss of attitude control on the second stage.

    References

    Long March 2C Wikipedia