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.
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Identity
- Aliases
- CZ-2C/SMLM-2C/SM长征二号丙SM
- Family Name
- Long March 2
- Full Name
- 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
- Parent Vehicle Family
- Rocket Specs
- Reusability
- expendable
- Stages Count
- 3
Links
Assets & Meta
- Creation Time
- July 17, 2026 at 05:00:10 UTC
- Updated Time
- July 19, 2026 at 11:44:33 UTC
- Image
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Other
- Search Name
- Long March 2C/SM CZ-2C/SM LM-2C/SM 长征二号丙SM