China's Space Program Thread II

by78

General
A better image that clearly shows the two test stands.

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That was fast. The new 700-ton engine test bench has just successfully completed its first engine test run. The engine used for the test run was the YF-100N (130-ton reusable LOX/Kerosene engine). The test bench has now been officially commissioned.

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The second test stand has also successfully completed its first engine run. With both test stands having been successfully tested and verified, the Tongchuan Test Center has achieved initial operating capability.

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by78

General
On April 17, Changguang Satellite Technology and OrienSpace held a signing ceremony for the "Jilin-1" high-resolution 05 satellite launch project in Beijing. OrienSpace will use its Gravity-1 rocket to launch Changguang's Jilin-1 05 remote-sensing satellite. OrienSpace will also provide Changguang with launch services for its next generation of remote-sensing satellite constellation.

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Gravity-1 all-solid launch vehicle developed by the private company OrienSpace will make its maiden flight in 2023. In 2025, Gravity-2 (re-usable liquid core + solid boosters) is scheduled to make first flight. In 2030, Gravity-3 (fully-reusable/recoverable) will make its maiden flight. Some 20 ground tests of various systems have been completed, including core stage engine for Gravity 1 and attitude control engines.

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On September 15, OrienSpace successfully completed a thermal test of the booster-stage solid rocket motor and servo mechanism for the Gravity-1 launch vehicle. Gravity-1 is expected to launch sometime next year.

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OrienSpace continues to perform ground tests on its Gravity-1 rocket, whose maiden flight is scheduled in Q4 of 2023. The company has recently completed noise tests as well as tests on the reaction control system of the final stage.

东方空间瞄准“引力-1号”火箭首飞成功目标,近期完成了十余项大型地面验证试验,其中噪声试验和末修姿控动力系统热试车试验的圆满完成,标志着火箭总体完成了全部初样研制工作,全力备战首飞任务。

噪声试验是“引力-1号”运载火箭系统级环境试验。火箭在发射飞行过程中会经受强烈的噪声环境,包括地面发射时火箭的排气噪声和高速飞行时的气动噪声等,可能会造成设备的损坏与失效,因此需在地面进行噪声环境的模拟试验对其进行考核。

试验中,按照飞行状态总装了箭体结构、航电系统、末修姿控动力系统,在末修姿控动力系统内填充了相关模拟介质,并对航电系统全程进行加电测试。本次试验达到了预期目标,对箭上结构件、电缆、管路、压力容器以及仪器设备等的环境适应性、振动环境下的工作可靠性进行了考核;获取了全面的数据,对火箭飞行过程中的声致振动环境条件设计进行了有效验证。

噪声试验后完成了冲击试验,随后末修姿控动力系统开展了综合热试车试验。“引力-1号”末修姿控动力系统为公司自主研制,采用4台50N和12台700N发动机,为火箭部分飞行过程提供反作用姿态控制(RCS)及卫星精确入轨所需的速度修正。

按照预定的试车程序,动力系统完成了电爆阀起爆、系统增压、电磁阀开关和推力室点火等所有动作,试车程序总时长约1200s,发动机最长稳态工作时间112s。试车过程中,气路和液路压力正常,电磁阀动作正常,推力室点火可靠,各单机匹配良好,参数指标符合预期;试车后,各单机状态完好,动力系统总装结构完好。

本次试车的圆满成功,充分验证了末修姿控动力系统设计的正确性和环境适应性,为“引力-1号”运载火箭的首飞成功奠定了坚实技术基础。
Oriental Space aimed at the successful first flight of the "Gravity-1" rocket, and recently completed more than ten large-scale ground verification tests, among which The successful completion of the noise test and the hot test of the final attitude control power system marks that the rocket has completed all the development of the initial prototype and is fully preparing for the first flight mission.

The noise test is a system-level environmental test of the "Gravity-1" launch vehicle. The rocket will experience a strong noise environment during launch and flight, including the exhaust noise of the rocket during ground launch and the aerodynamic noise during high-speed flight, which may cause damage and failure of the equipment. Therefore, it is necessary to conduct a simulation test of the noise environment on the ground Check it out.

During the test, the rocket body structure, avionics system, and final attitude control power system were assembled according to the flight status, and relevant simulation media were filled in the final attitude control power system, and the avionics system was powered on for the whole process. This test has achieved the expected goal, and the environmental adaptability of structural parts, cables, pipelines, pressure vessels, and instruments and equipment on the arrow, and the reliability of the work in a vibration environment have been assessed; comprehensive data has been obtained, and the rocket flight The design of acoustic-induced vibration environmental conditions in the process has been effectively verified.

After the noise test, the impact test was completed, and then the comprehensive thermal test was carried out for the final attitude control power system. The final attitude control power system of "Gravity-1" is independently developed by the company. It uses 4 sets of 50N and 12 sets of 700N engines to provide reaction attitude control (RCS) for part of the rocket's flight process and the speed correction required for the satellite's precise orbiting.

According to the scheduled test program, the power system has completed all actions such as detonation of the electric explosion valve, system pressurization, solenoid valve switch and thrust chamber ignition. During the test run, the air and liquid pressures were normal, the solenoid valves operated normally, the ignition of the thrust chamber was reliable, each unit was matched well, and the parameter indicators met expectations; after the test run, each unit was in good condition, and the power system assembly structure was intact.

The complete success of this test run has fully verified the correctness and environmental adaptability of the final attitude control power system design, and laid a solid technical foundation for the successful first flight of the "Gravity-1" carrier rocket.


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by78

General
According to CASC's official Weibo account, on May 23rd, China Satcom successfully demonstrated broadband internet connectivity in Jakarta, Indonedia using Zhongxing-26. During the demonstration process, the portable terminal completed the process from equipment assembly to satellite network connection within 120 seconds.



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Not sure if this is the same demonstration in Jakarta or a different one entirely.

近日,中国卫通配合工信部开展演示工作,本次演示使用我国首颗超百Gbps容量Ka高通量卫星——中星26号卫星。本次演示位于波束边缘,采用0.8米天线4W功放,实测下行速率达416Mbps,上传速率达8.32Mbps,为演示现场架设高速可靠的通讯“天路”,开启了我国高速卫星互联网服务新时代。

中星26号卫星宽带网络提供针对公专网及多场景的高速通信能力,单波束能力可达1.7Gbps,终端速率最高可达450Mbps,服务国土全境及“一带一路”重点区域。

Recently, China Satcom cooperated with the Ministry of Industry and Information Technology to carry out demonstration work. This demonstration uses my country's first Ka-band high-throughput satellite with a capacity of over 100 Gbps - Zhongxing 26 satellite. This demonstration is located at the edge of the beam, using a 0.8-meter antenna with a 4W power amplifier. The measured downlink rate reaches 416Mbps, and the upload rate reaches 8.32Mbps. It sets up a high-speed and reliable communication "sky road" for the demonstration site and opens a new era of high-speed satellite Internet services in my country.

The ChinaSat 26 satellite broadband network provides high-speed communication capabilities for public and private networks and multiple scenarios. The single-beam capability can reach 1.7Gbps, and the terminal rate can reach up to 450Mbps. It serves the entire territory of the country and key areas of the "Belt and Road".

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taxiya

Brigadier
Registered Member
It seems to me that an unmanned flight may make sense if the manned spacecraft and the lunar module are ready. Check all docking systems in lunar orbit. The module can perform landing operations by descending to a certain height. People will follow the already known path.
If you really want to make an unmanned mock landing, it is better to test the full stack with the lander landing and ascending then dock then separation then back, instead of a capsule and service module fly-by like what NASA did. China has did the lunar orbit manuvour and landing+returning procedures by Chang'e 5. All in all, China's development progress and steps are different from NASA, using NASA's practice isn't a good way to judge China's coming steps and time schedule.
 
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Kalec

Junior Member
Registered Member
CASC aims to run the first hot test of YF-91 in two years.


Machine translation:
2023年初,院所制定了2年内完成120吨级氢氧发动机整机试验考核的宏伟目标,多项阀门研制工作紧锣密鼓的展开。
At the beginning of 2023, the institute set the ambitious goal of completing the test and evaluation of the 120-ton hydrogen-oxygen engine within 2 years, and a number of valve development works were carried out in full swing.

在220吨级氢氧发动机研制工作中,作为阀门型号主管组长,抓总完成12种阀门关深研制,阀门通径、压力远大于以往型号产品。完成两次半系统试验、样机装配等标志性任务。

型号研制过程中突破了5项关键技术。阀门低温高压动密封技术将密封压力由16MPa提升至50MPa;金属硬密封技术成功研制出1000MPa高比压活门,得到了一种具有压力自紧效果的双道冗余密封,可实现近“零泄漏”,达国际先进水平;低温高压静密封技术将石墨圈密封挖潜至40MPa;低温高压动密封技术的突破摆脱了传统波纹管零泄漏设计理念,成本降低近60%;调节阀稳流技术研究实现了发动机推力精准控制,填补了我所在超低温液体流量调节领域的技术空白。
In the development of 220-ton hydrogen-oxygen engine, as the head of the valve development, he completed the development of 12 kinds of valve, and the valve diameter and pressure were much larger than the previous type products. Completed two semi-system tests, prototype assembly and other landmark tasks.

5 key technologies were broken through during the development of the model. Valve low-temperature high-pressure dynamic sealing technology to seal pressure from 16MPa to 50MPa; metal hard seal technology successfully developed 1000MPa high specific pressure valve, to get a pressure self-tightening effect of the double redundant seal, can achieve nearly "zero leakage", to the international advanced level; low-temperature high-pressure static sealing technology will The breakthrough of low-temperature and high-pressure dynamic seal technology has got rid of the traditional bellows zero-leakage design concept and reduced the cost by nearly 60%; the research of regulating valve flow stabilization technology has realized the precise control of engine thrust and filled the technical gap in the field of ultra-low temperature liquid flow regulation in our institute.


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