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| Attribute | Long March 6 (incl. 6A / 6C variants) 🇨🇳 China Trust: Operator-primaryⓘ Last verified Active · Last updated 2026-07-26Remove × | ||
|---|---|---|---|
| Company | CASC / CALT | SAST (Shanghai Academy of Spaceflight Technology) / CASC | United Launch Alliance |
| Country | 🇨🇳 China | 🇨🇳 China | 🇺🇸 USA |
| Status | Active | Active | Retired |
| Vehicle class | Heavy | Medium | Heavy |
| Propellant | LH₂ / LOX (YF-77 core) + RP-1/LOX (YF-100 boosters) | RP-1 / LOX (stages 1–2); N2O4/UDMH (stage 3, base variant) | LH2 / LOX |
| Reusable | No | No | No |
| Stages | 2 | 3 | 2 |
| First flight | 2016 | 2015 | 2004 – 2024 |
| Payload to LEO | 25,000 kgas of [1]CZ-5B variant (no upper stage) delivers 25,000 kg LEO for Tiangong station modules | 1,080 kg to SSO (base Long March 6)as of [1]Long March 6A (4 solid boosters, elongated stage 1): at least 4,000 kg to SSO. Long March 6C: similar class without the boosters. Both variants first flew from Taiyuan Satellite Launch Center. | 28,370 kgas of [1] ↑ Best |
| Payload to GTO | 14,000 kgas of [1]CZ-5 variant (with YF-75D upper stage) ↑ Best | — | — |
| Height | 56.97 mas of [1] | 29 m (base variant)as of [1] | 70.7 mas of [1] ↑ Best |
| Liftoff mass | 869 tas of [1] ↑ Best | 103 t (base variant)as of [1] | 733 tas of [1] |
| Success rate | 94.1%as of [2]16/17 successes (10 CZ-5 + 7 CZ-5B). Failure: CZ-5 Y2 (Jul 2017, engine anomaly); loss of Shijian-18 satellite. | 100% (base Long March 6, 15/15)as of [1]6A first flew 2022-03-29, 6C first flew 2024-05-07; both maintain perfect records within their own flight histories as of this date. ↑ Best | 93.75% (15/16 full success, 1 partial failure)as of [1] |
| Total flights | 17as of [2] ↑ Best | 15 (base variant)as of [1] | 16as of [1] |
| Cost / kg LEO | — | — | — |
| Summary | China's most powerful operational rocket and the backbone of its flagship space programs. Launched Tianwen-1 to Mars, Chang'e 5 sample return, Chang'e 6 far-side sample return, all Tiangong core and lab modules, and the Xuntian space telescope. The CZ-5B variant delivers entire station modules in a single flight. | A family of medium-lift launchers from SAST serving China's growing SSO/LEO commercial and government satellite demand, with the 6A and 6C variants adding solid boosters or a simplified expendable configuration respectively. | ULA's triple-common-booster-core heavy-lift launcher, retired 2024-04-09 after its final flight; superseded by Vulcan Centaur, which ULA states offers similar heavy-lift capability at lower cost. |
48 launch vehicles across 10 countries — active, retired, and in development — with primary-source citations from manufacturer user guides and agency press kits. Pure URL state: bookmark or share the link and the comparison reproduces exactly.