
At approximately 11 PM on April 8, 2026 Beijing time, the Long March 10B carrier rocket began erection at Launch Complex 2 of the CNSA – China National Space Administration- Hainan Commercial Space Launch Center, Hainan Province, China, People’s Republic of China. . This marks the first time a rocket other than the Long March 12 has been launched from Launch Complex 2.
According to the current plan, the Long March 10B carrier rocket will launch from Launch Complex 2 at the end of this month, marking the maiden flight of the Long March 10 series carrier rockets. It might be in consideration will send several satellites into orbit and attempt recovery not some kind of experiment.
So, what kind of awe will this large, bare-bones rocket, with a diameter comparable to the core stage of the Long March 5 and equipped with seven liquid oxygen/kerosene engines like the Long March 5

长征十号Long March 10 series rockets used for manned lunar landing and other missions successfully completed the test of the first-stage rocket power system. During the test, the engine started normally, worked stably, shut down at a fixed time, and all parameters were tested normally. This test is the first system-level large-scale ground test of the Long March 10 series of launch vehicles. The matching of the first-stage booster delivery system and the engine, the propellant filling process, the multi-machine parallel power transmission and environmental characteristics and other technologies were fully verified.








Long March 10 rocket is a three-and-a-half-stage rocket developed for the manned lunar exploration project. The total length of the rocket is 92.5 meters, the takeoff weight is about 2,189 tons, the takeoff thrust is about 2,678 tons, and the Earth-Moon transfer orbit carrying capacity is not less than 27 tons. In the future, it will be used to launch a new generation of manned spacecraft and lunar landers. In addition, the Long March 10 has also designed another booster-free configuration that can perform space station Takionaut and cargo transportation tasks….
The engine is the power source of the rocket, and its development process is very complicated. Test run is an important link in the engine development process, and there are dozens of types. In layman’s terms, engine test run is the process of igniting the engine and verifying the rationality of its design scheme and process reliability. This is an indispensable and important part of the development and delivery of a type 1 engine. It will run through all stages before and after engine development. Each stage of test run has different meanings, and the ignition time varies from a few seconds to hundreds of seconds.
It is reported that the engine used in this test run uses advanced liquid oxygen kerosene as fuel, which is improved and iterated from the high-thrust liquid oxygen kerosene engine used by the new generation of launch vehicles such as the Long March 5. The thrust reaches 130 tons. The R&D team of the Sixth Academy of Aerospace Science and Technology Group adheres to the concept of digital design, and has successively overcome key technical problems such as engine start-up and shutdown sequence, engine wide-range continuously variable thrust, and engine long life and high reliability.
In addition, the continuous success of the test run has fully verified the reliability of a number of new carrying process technologies. The engine production of this test run adopts the concept of intelligent manufacturing, and actively applies new materials, new processes, and new technologies. The inner wall of the thrust chamber of the core component adopts a new protective coating, key assemblies adopt automatic welding technology, and a large number of components adopt 3D printing technology.
The Long March 10 series carrier rockets are a new generation of manned carrier rockets developed by the First Academy of China Aerospace Science and Technology Corporation for manned lunar exploration missions. The tethered fire tests of the Long March 10 series of launch vehicles were conducted in a step-by-step, phased approach, focusing on two objectives: performance verification of the seven-engine, parallel-stage engine power system, and verification of recovery and reuse. These tests aimed to capture the true payload environment characteristics of the seven-engine, parallel-stage system and verify the recovery procedures. These tests were a key measure to mitigate risks associated with the maiden flight.
The grid fins and recovery hook on the top of a Long March 10 test rocket are clearly visible, while the bottom appears to have leading-edge fins (correction: it should be external piping), giving a glimpse of the future of marine net-system recovery…





t somewhat resembles the Hongshan Jade Dragon, but the lower half presents a reverse-curving posture, and there’s an extra stroke on the right. What would the complete version of the paint scheme look like
The Long March 10B carrier rocket is scheduled to make its maiden flight from 11:00 to 12:00 on April 28, 2026 , at the Wenchang Commercial Space Launch Site in Hainan. It will be the first to verify the world’s unique “sea-based net system recovery” technology and is expected to become China’s first carrier rocket to successfully enter orbit and be recovered.
I. Core Tasks and Technological Highlights
- First Flight Objectives and Innovative Recovery Plan
- A world-first net-based recovery system : The rocket’s first stage is equipped with grid fins and a high-strength hook. It uses retro-rockets to decelerate and re-enter the designated area in the South China Sea, where it is captured by the 144-meter-long recovery vessel “Navigator,” which carries a 36-meter-high “well”-shaped flexible arresting net, achieving a “soft landing” without the need for landing legs. This design reduces weight by 15%, lowers the requirements for engine thrust accuracy, and aims to reduce launch costs to a long-term target of 20,000 yuan/kg.
- Power and payload capacity : The rocket adopts a two-stage, bare-barrel configuration, with a body diameter of 5 meters and a total length of 69.67 meters. The core stage is powered by seven YF-100K/L liquid oxygen/kerosene engines in parallel (each with a thrust of 125 tons), providing a takeoff thrust of 892 tons. The second stage is equipped with one YF-219 liquid oxygen/methane engine . In recovered condition, it has a payload capacity of ≥16 tons to low Earth orbit at an altitude of 200 km and ≥11 tons to orbit at an altitude of 900 km, meeting the needs of satellite internet networking and lunar base construction
Images and visuals are from their Respectives CMS China Manned SpaceCNSA-China National Space Administration



















