Long March 2C
From Spacefaring
The Long March 2C (LM-2C), also known as the Chang Zheng 2C (CZ-2C), is a Chinese orbital launch vehicle, part of the Long March 2 rocket family. Developed and manufactured by the China Academy of Launch Vehicle Technology (CALT), the Long March 2C made its first launch on 9 September 1982. It is a two-stage launch vehicle with storable propellants, consisting of Nitrogen Tetroxide and Unsymmetrical Dimethylhydrazine. The launch vehicle was derived from the DF-5 ICBM.
Wikimedia, Wikidata
CZ-2C; Chang Zheng 2C; Changzheng-2C; LM-2C
Ashkenaz, Calvinist Republic of Ghent, Chinland, Democratic Republic of the Congo, Havilah, Kingdom of Martabam-hongsawatoi, Kingdom of Wolaita, China, Persia, Sikh Confederacy, Sweden, Tarshish, Dong Fang Hong 2, Ekran, 1982,
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Location: KML, Cluster Map, Maps,
| Type | Subtype | Date | Description | Notes | Source |
|---|---|---|---|---|---|
| commons | image | CZ-2C launch vehicle model | Commons | ||
| commons | image | Stack of 68 images (35min total) containing 39 Starlink, 3 GEO satellites and one rocket body | Commons | ||
| commons | image | Stack of 68 images (35min total) containing 39 Starlink, 3 GEO satellites and one rocket body | Commons | ||
| commons | image | Rendering of CZ-2C with two types of payload fairings (3.35 m and 4.2 m diameters) | Commons | ||
| commons | image | Rendering of CZ-2C with two types of payload fairings (3.35 m and 4.2 m diameters) | Commons | ||


