Long March 12B
| 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) reusable |
| Payload to SSO | |
| Altitude | 500 km (310 mi) |
| Mass | ~12,000 kg (26,000 lb) expendable |
| Associated rockets | |
| Family | Long March |
| Comparable | |
| Launch history | |
| Status | In development |
| Launch sites | JSLC LM-12 Pad |
| Total launches | 0 |
| First flight | NET February 2026 |
| First stage | |
| Powered by | 9 x YF102R |
| 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-102V |
| 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 planned 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 is anticipated to occur in 2026.