Long March 10B

Long March 10B
FunctionMedium-lift launch vehicle
ManufacturerChina Academy of Launch Vehicle Technology (CALT) of the China Aerospace Science and Technology Corporation (CASC)
Country of originPeople's Republic of China
Size
Height70.2 m (230 ft)
Diameter5 m (16 ft 5 in)
Stages2
Capacity
Payload to LEO
Altitude200 km (120 mi)
Mass16,000 kg (35,000 lb) with booster recovery
Payload to LEO
Altitude900 km (560 mi)
Mass11,000 kg (24,000 lb) with booster recovery
Associated rockets
FamilyLong March
Based onLong March 10
Comparable
Launch history
StatusActive
Launch sitesWenchang Commercial
Total launches1
Success(es)1
First flight10 July 2026
First stage
Powered by7 × YF-100K
Maximum thrustSL: 8,750 kN (1,970,000 lbf)
vac: 9,772 kN (2,197,000 lbf)
Specific impulseSL: 301.6 s (2.958 km/s)
vac: 337 s (3.30 km/s)
Burn time155 seconds
PropellantRP-1 / LOX
Second stage
Powered by1 × YF-219
PropellantCH4 / LOX

Long March 10B (LM-10B, Chinese: 长征十号乙; pinyin: Chángzhēng shí hào yǐ, CZ-10B) is a partially reusable two-stage medium-lift launch vehicle developed by China Rocket, the commercial launch subsidiary of China Academy of Launch Vehicle Technology (CALT). It is the third in the Long March 10 series of rockets and is derived using technologies developed for the Long March 10A.

Similar to the heavy-lift Long March 5, the CZ-10B stages have a five-meter diameter. Like other CZ-10 variants, the kerolox first stage is powered by seven YF-100K engines. The second stage uses one YF-219 methalox engine. Like other 21st century Long March designs, the CZ-10B launches from China's southernmost Wenchang Space Launch Site.

The CZ-10B's maiden flight in July 2026 successfully achieved orbit and booster recovery, using a net-based catching system on a floating landing platform in the South China Sea. This marked the first orbital booster recovery by the Chinese space program, the second country to achieve this after the United States, and the first recovery of any rocket using a net-based system.