Long March·China Aerospace Science and Technology Corporation
Long March 12A
Specifications
- Status
- active
- Height
- 69 m
- Diameter
- 3.8 m
- Stages
- 2
- Thrust
- 5,250 kN
- Payload to LEO
- 12,000 kg
- First flight
- 2025-12-23
- Total launches
- 1
- Success / Fail
- 1 / 0
Long March 12A/Changzheng 12A (LM-12A/CZ-12A) is a reusable orbital launch vehicle developed by the Shanghai Academy of Spaceflight Technology (SAST) of the state-owned China Aerospace Science and Technology Corporation (CASC). The rocket is based on the Long March 12, but extensively re-designed for first stage re-usability, and use of gas generator cycle methane/liquid oxygen powered rocket engines in both stages. The first stage uses 7 Longyun-70 engines designed and manufactured by the private company Jiuzhou Yunjian (JZYJ), while the second stage uses 1 YF-209V engine from CASC's Academy of Aerospace Liquid Propulsion Technology (AALPT). On launch missions where the first stage is recovered, it will land on a down-range landing pad located in Minqin County, Gansu Province.