#CNSA #ChinaNationalSpaceAdministration #国家航天局 |#BRI #June2024| #酒泉卫星发射中心 #JiuquanSatelliteLaunchCenter – #中国航天科技集团#ChinaAerospaceScienceAndTechnologyCorporation  – China’s first 10-kilometer-class vertical take-off and landing flight test of a #ReusableCarrierRocket was a complete success…

[China’s first 10-kilometer-class vertical take-off and landing flight test of a reusable carrier rocket was a complete success]

On June 23rd 2024, China’s first 10-kilometer-class vertical take-off and landing flight test of a reusable carrier rocket was a complete success. The rocket was developed by the Eighth Academy of China Aerospace Science and Technology Corporation.

 At about 1300 hours Beijing Time, at the Jiuquan Satellite Launch Center, Inner Mongolia, China, People’s Republic of China , a 3.8-meter-diameter reusable carrier rocket new technology verification arrow was erected on the launch pad. Three variable thrust liquid oxygen-methane engines were ignited, spewing blue tail flames. The rocket body rose to an altitude of about 12 kilometers. The central engine adjusted the thrust, and the rocket descended in a controlled manner. At 50 meters from the ground, the four landing legs unfolded, and then the rocket slowly descended, approaching zero altitude, and landed steadily on the recovery field, achieving a fixed-point vertical soft landing.


This test is currently the largest-scale vertical take-off and landing flight test of a reusable carrier rocket in China, and it is also the first application of the domestically developed deep variable thrust liquid oxygen-methane engine in a 10-kilometer-class return flight.
The entire test took about 6 minutes. The rocket went through five stages: accelerated ascent, decelerated ascent, accelerated descent, decelerated descent, and slow descent, achieving “take-off, accurate control, unfolding, and stable landing”.

[Take off, control accurately, deploy, and land steadily! China’s first 10-kilometer-level vertical take-off and landing flight test of a reusable carrier rocket was a complete success]

Three variable thrust liquid oxygen-methane engines were ignited, spewing blue tail flames. The rocket body rose to an altitude of about 12 kilometers. The central engine adjusted the thrust, and the rocket descended in a controlled manner. At 50 meters from the ground, the four landing legs unfolded, and then the rocket slowly descended, the altitude approached zero, and landed steadily on the recovery field, achieving a fixed-point vertical soft landing.



The entire test took about 6 minutes. The rocket went through five stages: accelerated ascent, decelerated ascent, accelerated descent, decelerated descent, and slow descent, achieving “take off, control accurately, deploy, and land steadily.”

The test fully verified the 3.8-meter diameter rocket body structure, large load landing cushioning technology, high-thrust strong variable thrust reusable engine technology, dual cryogenic pressurization delivery technology, high-precision navigation guidance control technology for return and landing, and health monitoring technology, laying a technical foundation for the first flight of a 4-meter-class reusable carrier rocket as scheduled in 2025. This test is currently the largest-scale vertical take-off and landing flight test of a reusable carrier rocket in China, and it is also the first application of the domestically developed deep variable thrust liquid oxygen-methane engine in a ten-Kilometer-class return..


The test fully verified the 3.8-meter-diameter rocket body structure, large-load landing buffer technology, large-thrust strong variable thrust reusable engine technology, dual low-temperature pressurization delivery technology, high-precision navigation guidance control technology for return and landing, and health monitoring technology, laying a technical foundation for the first flight of a 4-meter-class reusable carrier rocket as scheduled in 2025.


The apex of the flight profile of this test is the stratosphere at an altitude of about 12 kilometers. Subsequently, the research and development team will carry out a 70-kilometer-level vertical take-off and landing test of a reusable carrier rocket, which will basically cover the flight profile of the first stage of the rocket, and take another big step towards the goal of the first flight of a reusable carrier rocket.

Images and visuals are from their Respectives CMS China Manned SpaceCNSA-China National Space Administration

#MadeInChina #中國製造| #中科宇航 #ZhongkeAerospace #ChinaAcademyOfScience #CASSPace #June2024 | #CarrierRocket #ReusableCarrierRocket #CarrierRocket Series Lijian-2 China Aerospace Science and Technology has completed the joint test of the 85-ton kerosene #YF102  #CarrierRocketEngine in full flight conditions.  #ASummary

Beijing Zhongke Aerospace Exploration Technology Co., Ltd. is the first domestic aerospace enterprise with mixed ownership, and it is also the target enterprise that Oriental Aerospace Port focuses on introducing. Relying on the scientific research strength and resource advantages of the Institute of Mechanics of the Chinese Academy of Sciences and the Aerospace Flight Technology Center of the Chinese Academy of Sciences, China Aerospace Science and Technology has been committed to the research and development and integration of space technology and aerospace vehicles as a platform for the transformation of major national scientific research projects, as well as the transformation and provision of technological achievements. Aerospace launch service. The Lijian-1 rocket project also adds a brand-new name card to the Oriental Space Port, which will surely promote the construction of the Oriental Space Port to take a solid step forward.

On the Week of 17th June 2024 China Aerospace Science and Technology has completed the joint test of the 85-ton kerosene engine in full flight conditions.

Recently, China Aerospace Science and Technology has completed the joint test of the 85-ton liquid oxygen-kerosene engine and servo matching in the first stage of the Lijian-2 liquid carrier rocket. The test engine is in a two-way swing state, which can meet the control requirements of a 6-degree swing circle. The swing test simulating the full-scale operation of the first stage during the test was successful, verifying the matching of the first-stage engine of the Lijian-2 and the servo system, and obtaining key data such as the dynamic swing characteristics of the engine. At the same time, this test tested the first flight state of the first-stage engine of the Lijian-2.


This test assessed the two-way swing performance of the first-stage engine of the Lijian-2 and verified the working coordination of the servo control system and the engine. In the future, the engine will continue to carry out life test on this basis.
Lijian-2 adopts a CBC configuration, with a universal core stage diameter of 3.35 meters, a total length of 53 meters, a take-off weight of 625 tons, and a take-off thrust of 766 tons. The SSO carrying capacity is 8 tons, and the LEO carrying capacity is 12 tons. It is scheduled to fly for the first time in 2025…

[The joint test of the 85-ton liquid oxygen-kerosene engine YF-102 and servo matching flight conditions of the first stage of the Lijian-2 liquid carrier rocket of China Aerospace Science and Technology was successfully completed]

Recently, China Aerospace Science and Technology completed the joint test of the 85-ton liquid oxygen-kerosene engine and servo matching flight conditions of the first stage of the Lijian-2 liquid carrier rocket. The test engine is in a two-way swing state and can meet the 6-degree swing circle control requirements. The swing test simulating the full-scale operation of the first stage during the test process was successful, verifying the matching of the first stage engine of the Lijian-2 with the servo system, and obtaining key data such as the dynamic swing characteristics of the engine. At the same time, this test tested the first flight state of the first stage engine of the Lijian-2.


This test simulated the process of increasing the oxidizer and fuel inlet pressure caused by the flight overload of the first stage engine of the Lijian-2 by changing the engine inlet pressure. The engine thrust and specific impulse met the overall design requirements, the engine parameters were stable, and the performance indicators such as the oxygen self-pressurization met the design requirements.



During the test run, the engine extreme swing angle test, small swing angle joint training, load calibration, pressurized cold swing test, hot test combined swing test, etc. were carried out successively. During the ignition process, various waveform conditions such as square wave, triangle wave, and sine wave were tested. The maximum swing angle of the engine was 6°, and the servo feedback position and command tracking were good. The two-way swing performance of the first-stage engine of Lijian No. 2 was assessed, and the coordination between the servo control system and the engine was verified. Later, the engine will continue to carry out life survey tests on this basis.

Combined with this engine test run, liquid oxygen circuit immersion precooling, small flow precooling and large flow precooling tests were carried out simultaneously to obtain more accurate engine precooling characteristics and verify the correctness of the rocket body precooling scheme. In

addition, the low-order modal characteristics of the first-stage engine were obtained through structural modal tests of the installation process pull rod state and the installation servo mechanism state, providing important data support for the design of the attitude control system on the rocket. Environmental measurement points were added nearby to obtain environmental parameters such as noise.

Images and visuals are from their respectives

#CNSA #ChinaNationalSpaceAdministration #国家航天局 |#BRI #May2024 |#西昌衛星發射中心 #XichangSatelliteLaunchCenter the advance iconic #ChangZheng3B #LongMarch3B launches #Pakistan multi-mission #CommunicationSatellite #Satellites…..  #ASummary  

On the 30th May 2024 in  CNSA _China National Space Administration -China – People’s Republic of China 2012 hours Hong Kong –Beijing Time China- People’s Republic of China launch the Chang Zheng Long March 3B carrier rocket successfully launched the Pakistan multi-mission communications satellite…..  Satellite at the Xichang Satellite Launch Center, Sichuan Province

At 20:12 on May 30, the Long March 3B carrier rocket ignited and took off from the Xichang Satellite Launch Center, and then successfully sent the Pakistan multi-mission communications satellite into the predetermined orbit. The launch mission was a complete success. The Pakistan multi-mission communications satellite was developed by the Fifth Academy of China Aerospace Science and Technology Corporation and uses the Dongfanghong-4 enhanced communications satellite platform.

Pakistan’s multi-mission communications satellite
① Dongfanghong-4 enhanced communications satellite platform
② Equipped with 9 antennas and 48 C, Ku, Ka, L and other multi-band transponders
③ Take-off weight 5,400 kg
④ Fixed in geosynchronous orbit 38.2 degrees east longitude
⑤ Service life 15 years



The satellite has a service life of 15 years and will be stationed above the equator at 38.2 degrees east longitude in the geosynchronous orbit, covering Pakistan and surrounding areas. After in-orbit operation, the satellite will provide users in the region with a variety of services such as television, radio, regional enhanced communications, high-throughput broadband, and satellite-based enhanced navigation. The Long March 3B carrier rocket was developed by the First Academy of China Aerospace Science and Technology Corporation. This launch is the 524th launch of the Long March series of carrier rockets…

Images and visuals are from their Respectives CMS China Manned SpaceCNSA-China National Space Administration

#MadeInChina #中國製造| #中科宇航 #ZhongkeAerospace #ChinaAcademyOfScience #CASSPace #May2024 | #CarrierRocket #ReusableCarrierRocket #MannedReusableCarrierRocket #CarrierRocket Series Pulsating Production Model Lijian-1 Y4 Launch Vehicle Completes Final Assembly and Testing   #ASummary

Beijing Zhongke Aerospace Exploration Technology Co., Ltd. is the first domestic aerospace enterprise with mixed ownership, and it is also the target enterprise that Oriental Aerospace Port focuses on introducing. Relying on the scientific research strength and resource advantages of the Institute of Mechanics of the Chinese Academy of Sciences and the Aerospace Flight Technology Center of the Chinese Academy of Sciences, China Aerospace Science and Technology has been committed to the research and development and integration of space technology and aerospace vehicles as a platform for the transformation of major national scientific research projects, as well as the transformation and provision of technological achievements. Aerospace launch service. The Lijian-1 rocket project also adds a brand-new name card to the Oriental Space Port, which will surely promote the construction of the Oriental Space Port to take a solid step forward.

[Zhongke Aerospace Pulsating Production Model Lijian-1 Y4 Launch Vehicle Completes Final Assembly and Testing] Recently, Lijian-1 Y4 launch vehicle completed the final assembly and testing as scheduled at the Zhongke Aerospace Industrialization Base and successfully passed the factory review. Factory delivery conditions are met. This time is an example of starting a new chapter in the pulsating production model in an industrialized base and applying parallel assembly of multiple rockets. It fully verifies the leanness, standardization and mass production of rockets under the pulsating production model.

During the final assembly work of the Lijian-1 Yao-4 launch vehicle, based on the existing production process optimization basis, the task of starting the final assembly test of the Yao-4 and Yao-5 rockets in parallel was completed. At the same time, the Yaosi-4 Star-Arrow joint Operation test, satellite and rocket modal test, satellite and rocket separation test. The two rockets are located at different pulse production sites, and production resources are cleverly deployed at different production rhythm sites. On the one hand, it significantly improves the efficiency of production resource use, and on the other hand, it de-tasks rocket production and manufacturing. A solid foundation was laid.

In terms of process flow, technicians completed the relatively cumbersome process in the final assembly and testing phase, effectively reducing the final assembly workload at the launch site and facilitating the requirements for batch storage, rolling backup, and real-time launch during high-density launch periods. In terms of quality control, based on the accumulated successful practical experience of previous multiple missions, technical details have been continuously improved to form a complete closed-loop system for recording, monitoring, and tracking the entire process to ensure the traceability of the entire quality life cycle. Under the requirements of ensuring innovation in the production model and continuously improving product reliability, the final assembly of the Lijian 1 Yao 4 and Yao 5 launch vehicles was completed ahead of schedule. The final assembly of the Lijian 1 Yao 4 launch vehicle took 25 days, which was longer than the previous period. The speed of one-shot rocket assembly has increased again!

Under the pulsating production mode, the Lijian-1 Yao-6, Yao-7, and Yao-8 launch vehicles are carrying out mass production and final assembly in an orderly manner. The products, equipment, instruments, tooling, etc. involved in the entire process have been planned in advance. Deployment, production tasks are clear, and production and assembly can be started simultaneously in the final assembly and testing plant and intelligent manufacturing plant. It is worth mentioning that the Zhongke Aerospace Industrialization Base currently has complete structural cabin manufacturing and assembly capabilities. Starting from the Lijian-1 Yao-5 launch vehicle, the manufactured cabins will be directly used and delivered for final assembly, further shortening the production and manufacturing cycle. .

As China’s first medium-sized rocket to achieve high-density launches and the record holder for multiple satellite launches in a single launch of Chinese commercial rockets, the Lijian-1 carrier rocket has achieved complete success for three consecutive launches, accurately delivering 37 satellites with a total load of 3.5 tons into the scheduled orbit, with a 100% launch success rate. This type of rocket is suitable for rapid network launch of small and medium-sized satellites in medium and low orbits. It has a carrying capacity of 1.5 tons in a 500-kilometer sun-synchronous orbit. It is a medium-sized solid launch vehicle with core competitiveness in China’s commercial launch vehicle launch market and is also the main force in China’s commercial aerospace industry. It is one of the rockets that can effectively meet the needs of the commercial launch market in medium and low orbits. It also has the ability to respond quickly to diversified market demands and is committed to providing customers with highly reliable, low-cost, and high-density flight-based launch services.

Images and visuals are from their respectives

#MadeInChina #中國製造 #ExPace | #May2024 #CASIC Rocket Technology Company #Expace |#酒泉衛星發射中心#JiuquanSatelliteLaunchCenter #PrivateChineseSpaceCompany #Wuhan #CarrierRocketCompany #CarrierRocket #Kuaizhou11 #KX yao 4 successfully launch four adorable Four #Satellites #Wuhan1 #Tainyan22, #Lingque3

On the 21st May 2024 1215 Hong Kong SAR- Beijing Time, on the afternoon of, China, People’s Republic of中國製造 Expace Technology Corporation, China Aerospace Science and Industry Corporation’s Aerospace Sanjiang Rocket Company was a complete success launched Kuaizhou 11 successfully opened a new phase of batch launch!

At 12:15 on May 21, 2024, the “Kuaizhou 11” Yaosi-4 launch vehicle carried the main satellite “Wuhan-1” satellite, the ultra-low orbit technology test satellite and the carrying satellites Tianyan 22 and “Lingque 3” Four satellites of magnitude 01 were ignited and launched from station 95A of the Jiuquan Satellite Launch Center, placing the satellites into predetermined orbits.

Kuaizhou 11 (KZ-11) is a medium-sized solid launch vehicle developed by China Aerospace Science and Industry Corporation’s Aerospace Sanjiang. It adopts a four-stage series configuration, with the first, second and third stages using solid power and the fourth stage using liquid power. The rocket has a height of 25 meters and a diameter of 2.2 meters. It can be equipped with fairings of 2.2 meters in diameter and 3.2 meters in diameter. It has a take-off mass of 78 tons and a take-off thrust of 180 tons. Its low-Earth orbit (LEO) transport capacity is 1.5 tons and its range is 700 kilometers. Sun-synchronous orbit (SSO) capacity 1 ton. This rocket is equipped with a fairing with a diameter of 2.2 meters.

Since its first flight (failed) on July 10, 2020, the Kuaizhou-11 has carried out a total of three launches, with a success rate of about 67%. Starting this year, the Kuaizhou-11 has entered the batch launch phase, with plans to carry out no less than four launch missions, with the target orbit being a sun-synchronous orbit (SSO) at an altitude of 530 kilometers.

This launch is the first launch of the Kuaizhou-11 rocket in 2024, the 8th launch of the Jiuquan Satellite Launch Center, the 24th launch in China, and the 96th launch in the world.

Images and visuals are from a their respectives..