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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

2016 Vol. 17, No. 3 Published:09 September 2016
Electrodynamic Tethered Deorbit System Dynamics and Performance Analysis
ZHANG Feng, SHEN Lin, WU Shengbao, WANG Xiaoding, WANG Shuting, YU Bensong
2016, 17(3):  3-11. 
Abstract ( 233 )   PDF (786KB) ( 239 )  
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Electrodynamic tethered deorbit technology is a novel way to remove abandoned spacecrafts like upper stages or unusable satellites. This paper investigates and analyses the deorbit performance and mission applicability of the electrodynamic tethered system. To do so, the electrodynamic tethered deorbit dynamics with multi-perturbation is firstly formulated, where the Earth magnetic field, the atmospheric drag, and the Earth oblateness effect are considered. Then, the key system parameters, including payload mass, tether length and tether type, are analyzed by numerical simulations to investigate their influences on the deorbit performance and to give the setting principles for choosing system parameters. Based on this and given an appropriate group of system parameters, numerical simulations are undertaken to study the impact of the mission parameters, including orbit height and orbit inclination, and thus to investigate the mission applicability of the electrodynamic tethered deorbit technology.
Maiden Flight of Long March 7-The New Generation Medium Launch Vehicle in China
WANG Xiaojun, FAN Ruixiang, CHENG Tangming, XU Lijie, YANG Haoliang
2016, 17(3):  12-18. 
Abstract ( 270 )   PDF (951KB) ( 321 )  
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On June 25, 2016, the Long March 7 (LM-7) launch vehicle completed its maiden flight successfully. 
LM-7, as a new generation of medium and basic launch vehicle based on the design concepts of non-toxic and nonpolluting, was developed for the purpose of launching a cargo spacecraft to the Chinese space station. Based on the experience on launching cargo spacecraft and satellites, LM-7 can be adapted for mainstream satellite launch missions in the future with its characteristics of serialization and continuous optimization. LM-7 is expected to be used to launch manned spacecraft in the future. This paper presents a general review of LM-7 with regard to the general scheme and provides references for the development prospects of a medium launch vehicle series in China.
Development Prospect of the Commercialization for Aerospace Services
WANG Guoqing
2016, 17(3):  19-27. 
Abstract ( 206 )   PDF (399KB) ( 264 )  
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In recent years, with the rapid growth in demand for commercial launches, space institutions like NASA have been succeeded in the commercialization of aerospace services. According to the latest development trends on international commercial aerospace services and the current development status of domestic commercial aerospace services, suggestions on the development of China’s commercial aerospace services based on policies, development modes and technical innovation are given.
The Influence of Quantum Technology on the Development of Metrology and Measuring Science
ZHANG Tieli, MIAO Yinxiao
2016, 17(3):  28-35. 
Abstract ( 237 )   PDF (417KB) ( 266 )  
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In the new century, quantum technology has developed rapidly and has been applied in many fields. As an important aspect of the aerospace science, metrology and measuring science is a field which is influenced by the quantum technology dramatically. The new generation of the International System of Units will be redefined on the basis of the quantum theory. More and more new sensing techniques are developed taking into account quantum principles. In this paper, the influence of quantum technology on metrology and measuring science is introduced.
Technology and Market Prospect Analysis of Low Cost Small-lift Launch Vehicles for Small Satellites
YAO Yanfeng, CUI Yinghui, FAN Wei, PEI Shengwei
2016, 17(3):  36-43. 
Abstract ( 232 )   PDF (296KB) ( 331 )  
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The technological development status of new generation low cost small-lift launch vehicles applied to small satellite launch is investigated in this paper. The development trends are summarized, including low cost and rapid response capability, utilization of mature rocket and missile technology, the development of mobile launch technology adopting air-based platforms and use of innovative technology. Moreover, the external power and internal demand of the small-lift launch vehicle are analyzed and the market prospect is forecasted. Finally, proposals for the development of small-lift launch vehicles are put forward, including exploration of the potential of existing rocket and missile technology, development of multi-platform mobile launch technology and further application of innovative technology and ideas.
Frontier Research in Hand, National Demands in Mind
2016, 17(3):  44-47. 
Abstract ( 199 )   PDF (480KB) ( 22 )  
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Three Major Tasks of The Tiangong 2 Space Laboratory
WEI Jinghua
2016, 17(3):  48-50. 
Abstract ( 194 )   PDF (247KB) ( 255 )  
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CRESDA Successfully Processed the First Track Data of GF-3
2016, 17(3):  51-53. 
Abstract ( 136 )   PDF (1147KB) ( 20 )  
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LM-2F Carries out Shenzhou 11 Mission Successfully
YAO Tianyu
2016, 17(3):  54-54. 
Abstract ( 155 )   PDF (355KB) ( 224 )  
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China’s First Space Laboratory Tiangong 2 Was Launched into Space Successfully
WEI Jinghua
2016, 17(3):  55-55. 
Abstract ( 149 )   PDF (251KB) ( 196 )  
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China Launches First Quantum Science Satellite
WANG Juan
2016, 17(3):  56-56. 
Abstract ( 160 )   PDF (259KB) ( 185 )  
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A LM-4C Launches the GF-3 Satellite
YAO Tianyu
2016, 17(3):  57-57. 
Abstract ( 168 )   PDF (517KB) ( 184 )  
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LM-3B Launches Tiantong 1 Satellite
XIE Ruiqiang
2016, 17(3):  58-58. 
Abstract ( 162 )   PDF (379KB) ( 236 )  
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China Will Launch 14 Meteosats over the Next Ten Years
YAO Tianyu
2016, 17(3):  58-58. 
Abstract ( 1 )   PDF (379KB) ( 7 )  
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FY-4 Satellite Prepares for Launch at XSLC
JIANG Shengguang/ZHOU Xia
2016, 17(3):  59-59. 
Abstract ( 155 )   PDF (361KB) ( 284 )  
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China Unveils Its First Mars Probe and Rover
YAO Tianyu
2016, 17(3):  60-60. 
Abstract ( 136 )   PDF (357KB) ( 212 )  
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Hollow Cathode Life Test for Electric Thruster Achieves Breakthrough
QIAO Caixia
2016, 17(3):  61-61. 
Abstract ( 2 )   PDF (81KB) ( 8 )  
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500-ton LOX/Kerosene Engine Joint Test Achieved Success
ZHANG Ping
2016, 17(3):  63-63. 
Abstract ( 200 )   PDF (82KB) ( 226 )  
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3 m Twin-Segment Solid Rocket Engine Tested Successfully
YAO Tianyu
2016, 17(3):  63-63. 
Abstract ( 4 )   PDF (82KB) ( 9 )  
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Lao Satellite Concession Agreement Signed
HUANG Haiyan
2016, 17(3):  64-64. 
Abstract ( 191 )   PDF (548KB) ( 224 )  
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