Long March 2C/SM
Long March 2C/SM was a three-stage Long March 2C configuration developed for the China-ESA Double Star scientific mission. It flew twice, launching Tan Ce 1 to an equatorial orbit in 2003 and Tan Ce 2 to a polar orbit in 2004.
Identity
- Aliases
- CZ-2C/SMLM-2C/SM长征二号丙SM
- Family Name
- Long March 2
- Full Name
- Long March 2C/SM
- Reusability
- expendable
- Slug
- long-march-2c-sm
- Status
- retired
- Type
- rocket
- Variant Name
- C/SM
Details
- Description
- Long March 2C/SM was a three-stage Long March 2C configuration developed for the China-ESA Double Star scientific mission. It flew twice, launching Tan Ce 1 to an equatorial orbit in 2003 and Tan Ce 2 to a polar orbit in 2004.
- First Flight Year
- 2,003
- Last Flight Year
- 2,004
- Manufacturer Id
- jd7fbrt32syts4rtsgsh4m023n7kqwpa
- Parent Vehicle Family Id
- nd7washgysptatw85f3zfzpyj98ah7yn
- Stages Count
- 3
Links
Assets & Meta
- Creation Time
- 7/17/2026, 5:00:10 AM
- Updated Time
- 7/17/2026, 5:01:03 AM