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AEROSPACE CHINA

Sponsored by

China Aerospace Science and Technology Corporation

Published by

China Aerospace Academy of Systems Science and Engineering

ISSN 1671-0940

CN 11-4673/V

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AEROSPACE CHINA

Sponsored by

China Aerospace Science and Technology Corporation

Published by

China Aerospace Academy of Systems Science and Engineering

Published quarterly in Spring, Summer, Autumn and Winter

Address: Room 403, No.16 Fucheng Rd., Beijing 100048, PR China

ISSN 1671-0940

CN 11-4673/V

AEROSPACE CHINA

AEROSPACE CHINA

2020 Vol. 21, No. 1 Published:01 May 2020
Research Articles
The CSES Mission and Its Preliminary Results
SHEN Xuhui , ZEREN Zhima , YUAN Shigeng , DAI Jianping , HUANG Jianping , ZHU Xinghong , YANG Yanyan , YAN Rui , ZHAO Shufan , LIU Dapeng , ZHANG Zhenxia , WANG Qiao , CHU Wei , LU Hengxin , XU Song , GUO Feng , TAN Qiao , LI Wenjing , ZHOU Na
2020, 21(1):  5-18.  doi:10.3969/j.issn.1671-0940.2020.01.001
Abstract ( 448 )   PDF (3450KB) ( 319 )  
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satellite of the China national geophysical field observation series of satellite missions, the China Seismo-Electromagnetic Satellite (CSES) was designed upon an optimized CAST2000 platform for a sun synchronous orbit. Onboard CSES, there are total eight types of scientific payloads including the Search-coil Magnetometer, Electric Field Detector, High Precision Magnetometer, GNSS Occupation Receiver, Plasma Analyzer, Langmuir Probe, Energetic Particle Detector Package, and a Three-band Transmitter to individually acquire the global electromagnetic field, electromagnetic waves, ionospheric plasma parameters as well as energetic particles. Up to now, CSES has been operating normally in orbit for 2 years. By using the various sensor data acquired by CSES, we have achieved scientific research in the areas of the global geomagnetic field modeling, space weather, earthquake event analysis, the Lithosphere-Atmosphere-Ionosphere coupling mechanism and so on.
Analysis and Solution for Excessive Radiated Emission with a Certain Type of Laser Scanner
HOU Yanchun, ZHANG Qian, YANG Xue, SHI Yanchao, LV Changchun
2020, 21(1):  19-25.  doi:10.3969/j.issn.1671-0940.2020.01.002
Abstract ( 220 )   PDF (2223KB) ( 189 )  
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The problem of excessive radiated emission for a certain type of laser scanner is discussed in this paper.
Firstly, the frequency characteristics of the laser scanner can be obtained by traditional test methods. According to the
frequency and electronic equipment characteristics, the interference source can be estimated and established. Then
based upon analysis, modified methods are proposed. By applying the above methods, the interference source can be
identified and the amount of radiated emission from the scanner can be reduced effectively. Finally, the scanner can op
erate in a compatible manner with other electronic systems at the same time. The above methods can provide a ref
erence for electronic equipment design ensuring electromagnetic compatibility and passing the radiated emission test.
Reviews
Lunar Exploration and Development Vision
SUN Weigang , WANG Zhaoqi , ZHAO Qi
2020, 21(1):  26-32.  doi:10.3969/j.issn.1671-0940.2020.01.003
Abstract ( 283 )   PDF (1079KB) ( 241 )  
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By summarizing the history, human achievements in lunar exploration, the vision and prospect of the construction of a lunar base for the further development in lunar exploration is proposed. The idea of building a “beehive” lunar village is proposed, and the promotion of future lunar exploration along with the impact on the development of science, technology and the economy is analyzed in this paper.
Review on Technical Characteristics and Development Laws of Solid Launch Vehicles
BU Xiangwei , YANG Haoliang , SHI Xiaoning , WEI Kai , YANG Yiqiang
2020, 21(1):  33-42.  doi:10.3969/j.issn.1671-0940.2020.01.004
Abstract ( 301 )   PDF (1369KB) ( 364 )  
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Solid-propellant and liquid-propellant launch vehicles have their own characteristics, both playing an important role in space ransportation systems of space powers. This paper reviews and summarizes the development history of solid-propellant launch vehicles, and analyzes their technical characteristics including multiple stages, large payloads, complex separation, diverse operation modes, fast response, and mission adaptability as well as unique advantages in launch ctivities. This paper analyzes and proposes four development laws for solid-propellant launch vehicles, including improving omprehensive performance, infusing heritage with innovation, unitization and seriation, and optimizing power systems. Finally, this paper proposes the opportunities and challenges faced by solid-propellant launch vehicles based on market demands.
SPACE POLICY
Moving Towards a Potential Conflict Resolution Mechanism Under the APSCO Framework: A Proposed Legal Mechanism
Mohammad Saiful Islam
2020, 21(1):  43-52.  doi:10.3969/j.issn.1671-0940.2020.01.005
Abstract ( 334 )   PDF (310KB) ( 197 )  
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Competition among countries has evolved from just on Earth but into space as space technology and space power is a key attribute in the world today. Today space technology has spread, due to the enormous development, into every sector of life in the Earth for the benefit of mankind. Every country has the ambition to be a part of the space initiative. Asia Pacific Space Cooperation Organization (APSCO) is an organization that tries to promote space activities through cooperation in the Asia Pacific region. This paper attempts to explore the nature and categories of potential conflict that may arise under the APSCO framework program. Furthermore, it also endeavors to establish an effective and better dispute settlement mechanism under the overall APSCO framework. Finally, this paper introduces the institutional framework and working procedures of the arbitration body for future smooth cooperation and space exploration by APSCO.
News in Brief
China Launches Yaogan-30 06 Group of Satellites
MIAO Shanshan
2020, 21(1):  55-55. 
Abstract ( 227 )   PDF (389KB) ( 172 )  
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LM-2D Launches 4 New Technology Experimental Satellites
ZHAO Cong
2020, 21(1):  57-57. 
Abstract ( 181 )   PDF (567KB) ( 158 )  
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LM-2D Successfully Launches 4 Satellites into Orbit on One Launch
TANG Mingjun
2020, 21(1):  58-59. 
Abstract ( 170 )   PDF (776KB) ( 208 )  
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China’s First Flight of DFH-5 Satellite Platform Succeeds
ZONG Wen
2020, 21(1):  60-60. 
Abstract ( 207 )   PDF (142KB) ( 237 )  
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