China's Space Program Thread II

by78

General
Zhongke has successfully completed a engine test run on its newly constructed liquid engine test bench. The performance parameters of the test bench have met all design requirements.

The engine tested was the company's 30-ton LOX/Kerosene engine. Does anyone know anything more about this engine?

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by78

General
An academic paper on the 1.5tf (15kN) main engine for China's new manned spacecraft that will be used for landing on the moon. The engine has passed both ground and high-altitude hot test runs, with its performance parameters meeting all design requirements. The engine has demonstrated a single run duration of 1000 seconds in ground tests. In high-altitude tests, it has achieved nine consecutive engine start-stops and single run duration of 100 seconds.

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Abstract: 1.5 tf再生冷却液体火箭发动机用于我国载人登月新一代载人飞船主动力,具备高可靠、高比冲和多次点火启动等能力。头部采用多组喷注单元同心圆排列的直流互击式喷注器,身部燃烧室采用增材制造中逐层熔覆的激光选区熔化技术制备,喷管延伸段采用轻质C/SiC复合材料制备,两者通过螺栓、法兰连接和柔性石墨密封。采用再生冷却、液膜冷却和辐射冷却的组合热防护方式加强身部冷却效果,双密封联动的低流阻气动电磁阀控制推进剂流动。通过设计和工艺联合攻关,初步突破了高性能稳定燃烧和可靠冷却、再生冷却身部一体化增材制造、大尺寸复合材料喷管成形和连接等关键技术,通过了地面热试车和高空模拟热试车验证。发动机工作稳定,再生冷却温升裕度大,实测真空比冲为315.3 s,达到相同系统参数下国际先进水平,主要技术指标满足设计要求,为后续工程研制奠定了坚实的技术基础。

The 1.5 tf liquid rocket engine with regenerative cooling is used as the main power of China's next-generation manned spacecraft for manned lunar landing, which has the capability of high reliability, high specific impulse and multiple ignitions. The engine head is an unlike impinging injector with multiple injection units arranged in concentric circles. The combustion chamber is prepared by selective laser melting technology with layer-by-layer fusion in additive manufacturing, and the nozzle extension is prepared by lightweight C/SiC composite material, both of which are connected by bolts, flanges and flexible graphite seals. The combined thermal protection mode of regenerative cooling, liquid film cooling and radiation cooling is used to enhance the cooling effect of the body, and the propellant flow is controlled by the low flow resistance and double-seal linkage pneumatic solenoid valve. Through joint research on design and process, key technologies such as high-performance stable combustion and reliable cooling, integrated additive manufacturing of regenerative cooling body, forming and connecting large-size composite material nozzle have been preliminarily broken through, which have been verified by the ground thermal test and high-altitude simulation hot-fire test. The engine operates stably, with a large margin for regenerative cooling temperature rise. The measured vacuum specific impulse of the engine is 315.3 s, reaching the international advanced level under the same system parameters. The main technical indexes meet the design requirements, laying a solid technical foundation for the subsequent engineering development.

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stoa1984

Junior Member
Registered Member
As explained in my previous posts, the Chinese long term space resources plan spanning the entire Solar System, now officially disclosed to the public.

Wang Wei presented this at a Chinese Society of Astronautics meeting in Beijing on 19th August 2023, in a forum on 'Exploring the Universe and Developing Space Resources' (中国宇航学会第一届空间科学与试验学术交流会).

天工开物
2023-08-20
Wang Wei, affiliated to CASC & CAS, is proposing a four-stage roadmap for creating a space resources utilization system spanning the entire Solar System. Far-sighted, ambitious to say the least.
The initiative is called "天工开物" Tiangong Kaiwu, taking its name from Ming Dynasty scientist Song Yingxing's work "The Exploitation of the Works of Nature."
Water as fuel: proposes development of strategic mineral resources as the goal, based on utilization of space water-ice resources, using Lagrangian points 1+2 b/w celestial bodies as nodes & build a gradually build space resource development system out into the Solar System.
Plan is to gradually construct water-ice resource development facilities on the moon, NEAs, Mars, main-belt asteroids & moons of Jupiter satellites, and gradually form a system using Earth-Moon L1, Sun-Earth L1/L2, Sun-Earth L1/L2, Ceres, and Sun-Jupiter L1.
This requires resource infrastructure inc. supply stations, transportation routes, mining & processing stations, and focus on access space, low-cost return to Earth, key tech, etc, to develop large-scale and commercial space resource development & utilization capabilities.
This notion has stage goals of "exploration, mining, and utilization" with stage posts at 2035, 2050, 2075 & 2100. This will "promote the development and utilization of space resources in my country to achieve leapfrogging style development," says Wang.
Wang: "Just like the miracles created in the Age of Great Navigation, the 'great space age' the development of space resources will create the next miracle in the history of human development and bring new prosperity to human civilization."
There's lots to consider regarding this, such as what level of support it can attain, China's budgets and economy, technological and economic feasibility, and how this works within the Outer Space Treaty, and many different interpretations from outside.
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▲ Academician Wang Wei made a special report on "Development Vision of Space Resource Development System". 王巍院士作《太空资源开发体系发展设想》特邀报告
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This begs the question, which new space launchers could be used to develop the asteroid belt, Ceres and Jupiter?

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:D
 

iantsai

Junior Member
Registered Member
北京时间2023年8月31日15时36分,我国在西昌卫星发射中心使用长征二号丁运载火箭,采取一箭三星方式,成功将遥感三十九号卫星发射升空,卫星顺利送入预定轨道,发射任务获得圆满成功。

此次任务是长征系列运载火箭第485次飞行。
China successfully launched Yaogan-39 Group-1's three satelites by a CZ-2D rocket from Xichang Satelite Launch Center in 15:36 UTC+8, August 31, 2023.

This is the 485th CZ series rocket launch.

A launch yesterday that no one mentioned;)
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