CZ-10 (Chang Zheng-10)

CZ-10 []

CZ-10A []

CZ-10A Abort test []

CZ-10B (Y1) []

The CZ-10 carrier rocket is a Chinese heavy-lift launch vehicle being developed by the Shanghai Academy of Spaceflight Technology based on the CZ-5 rocket.

It will be able to place at least 70 tons of payload in low Earth orbit and at least 27 tons into a lunar transfer orbit orbit. Its initial launch is scheduled for 2026 from Hainan.

Version Strap-On Stage 1 Stage 2 Stage 3
CZ-10 2 × CZ-10-0 / 7 × YF-100K CZ-10-1 / 7 × YF-100K CZ-10-2 / 2 × YF-100M CZ-10-3 / 3 × YF-75E
CZ-10A - CZ-10-1 / 7 × YF-100K/L/N CZ-10A-2 / YF-100M -
CZ-10A (1 stage) - CZ-10-1 (short) / 7 × YF-100K/L/N - -
CZ-10B - CZ-10-1 / 7 × YF-100K/L/N CZ-10B-2 / YF-219 -
CZ-10B - CZ-10-1 / 7 × YF-100K/L/N CZ-10B-2 / YF-219 -
CZ-10C - CZ-10C-1 / 7 × YF-219 CZ-10B-2 / YF-219V -
Performance (kg) LEO LPEO SSO GTO GEO MolO IP
CZ-10 70000 27000
CZ-10A 14000 - - -
CZ-10A(ex) 18000 - - -
CZ-10B 16000 11000 - - -
CZ-10B(ex) 18000 - - -
No:       Type:              Serial    Date            LS            Payload

 1    1   CZ-10A (1 st)      .         11.02.2026 *    We LC-301     Mengzhou Abort Capsule
 2    1   CZ-10B             .         10.07.2026      HCS LP-2      CX 26
 

Planned:

      1   CZ-10A             .         xx.xx.2026      We LC-301     Mengzhou 1


Launch sites:

HCS =    Hainan Commercial Spaceport, Hainan, China   China
We  =    Wenchang Space Launch Center (WSLC), Hainan, China   China


F       Failure
P       Partial Failure

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