Long March 6C

The Long March 6C (CZ-6C) is a Chinese two-stage-to-orbit liquid-fueled launch vehicle designed and manufactured by Shanghai Academy of Spaceflight Technology, a subsidiary of China Aerospace Science and Technology Corporation. The rocket is a dual engine first stage variant of the Long March 6; alternatively, it may be considered to be a slightly shorter single stick variant of the Long March 6A. Both the first and second stages of the rocket use liquid oxygen and RP-1 propellants. It is employed to launch small and medium-sized military, civilian and commercial satellites to LEOs and Sun-synchronous orbits; it is capable of lifting 2,400 kg to 500 km SSOs.

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