| Function | Medium-lift to heavy-lift launch vehicle |
|---|---|
| Manufacturer | China Aerospace Science and Technology Corporation Commercial Rocket Co., Ltd. |
| Country of origin | China |
| Size | |
| Height | ~72 m (236 ft 3 in) |
| Diameter | 4.37 m (14 ft 4 in) |
| Mass | > 437,000 kg (963,000 lb) |
| Stages | 2 |
| Capacity | |
| Payload to LEO | |
| Altitude | 200 km (120 mi) |
| Mass | ~20,000 kg (44,000 lb) expendable, 12,000 kg (26,000 lb) reusable1 |
| Payload to SSO | |
| Altitude | 500 km (310 mi) |
| Mass | ~12,000 kg (26,000 lb) expendable1 |
| Associated rockets | |
| Family | Long March |
| Comparable | |
| Launch history | |
| Status | Active |
| Launch sites | Jiuquan, CZ-12 pad |
| Total launches | 1 |
| Success(es) | 1 |
| Failure | 0 |
| First flight | 1 June 2026 |
| First stage | |
| Powered by | 9 × YF102R2 |
| Maximum thrust | 7,515 kN (1,689,000 lbf) |
| Specific impulse | 275.3 seconds (2.700 km/s) |
| Propellant | RP-1 / LOX |
| Second stage | |
| Powered by | YF-102V2 |
| Maximum thrust | 835 kN (188,000 lbf) |
| Propellant | RP-1 / LOX |
The Long March 12B (Chinese: 长征十二号乙运载火箭; pinyin: Chang Zheng 12B, abbreviated LM-12B or CZ-12B), is a Chinese reusable medium-lift to heavy-lift launch vehicle. The rocket has two stages and its first stage is designed to be reused after stage-recovery via propulsive landing. Both stages of the rocket will use kerosene and liquid oxygen (LOX) for propulsion. The rocket is being developed by the China Aerospace Science and Technology Corporation Commercial Rocket Co., Ltd. (CACL), operating under the state-owned China Aerospace Science and Technology Corporation (CASC). The first flight of the rocket was conducted successfully on 1 June 2026.3
History
CACL has described the CZ-12B as a 4-meter-diameter class rocket that will use a kerosene and liquid oxygen propellant mix, unlike the CZ-12A which use methane and liquid oxygen. CACL further describes the CZ-12B as having a “20-ton-class low Earth orbit carrying capacity”, this is likely in an expendable mode.4
A static fire test of the rocket's first stage occurred on 16 January 2026 at the Dongfeng Commercial Space Innovation Test Zone within the Jiuquan Satellite Launch Center in northwest China. First launch of the rocket is expected to occur in 2026.4
The first launch of the CZ-12B occurred on 1 June 2026; the mission was a success and placed the 08 Group of the Qianfan Constellation into polar orbits.3
Launch statistics
- Failure
- Partial failure
- Success
- Planned
List of launches
| Flight | Launch (UTC) | Payload | Orbit | Launch site | Outcome | Booster recovery |
|---|---|---|---|---|---|---|
| Y1 | 1 June 2026 08:403 |
Qianfan Polar Group 08 | Polar | Jiuquan, CZ-12 pad | Success | Not attempted |
| First flight of the CZ-12B. First stage recovery was not attempted. | ||||||
See also
See also
References
References
- "Re: Inaugural launch - CZ-12B - JSLC - NET(?) March or before late January (Reply #2)". nasaspaceflight.com. 16 January 2026. Retrieved 16 January 2026.
- C, Jack (17 January 2026). "Reusable Long March 12B fires up ahead of first flight". china-in-space.com. Retrieved 17 January 2026.
- 李, 国利; 王, 晨宇 (1 June 2026). "长征十二号乙遥一运载火箭发射成功". XINHUAnet.com. Retrieved 1 June 2026.
- Jones, Andrew (16 January 2026). "China conducts static fire test of new reusable Long March 12B rocket". spacenews.com. Retrieved 16 January 2026.