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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Long March 6, 
Ashkenaz, Calvinist Republic of Ghent, Chinland, Democratic Republic of the Congo, Havilah, Kingdom of Martabam-hongsawatoi, Kingdom of Wolaita, Persia, Sikh Confederacy, Tarshish, Dong Fang Hong 2, Ekran, Long March 6, Republic of Haiti, 

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长征六号丙运载火箭首飞成功.mkv 20251024 160656.743

长征六号改系列火箭模拟图

长征六号丙运载火箭首飞成功.mkv 20251024 160656.743

Type	Subtype	Date	Description	Notes	Source
commons	image		长征六号丙运载火箭首飞成功.mkv 20251024 160656.743		Commons
commons	image		长征六号改系列火箭模拟图		Commons
commons	image		长征六号丙运载火箭首飞成功.mkv 20251024 160656.743		Commons