PMO OpenIR
progressinspacedebrisresearch
Zhao Changyin1; Zhang Wenxiang2; Han Zengyao3; Wang Hongbo1
2010
Source Publication空间科学学报
ISSN0254-6124
Volume30Issue:5Pages:516
AbstractDuring recent years,A de-orbit disposal of Sino Sat 2 satellite and the depletion of the residual propellant after SC/LV separation for all LM-4 series launch vehicles were carried out. Stuffed Whipple Shields based on hypervelocity impact particles were developed. Routine observation and collision avoidance were performed. The main progress in space debris research will be introduced from three aspects:mitigation, spacecraft protection, observation and collision avoidance
Language英语
Document Type期刊论文
Identifierhttp://libir.pmo.ac.cn/handle/332002/29835
Collection中国科学院紫金山天文台
Affiliation1.中国科学院紫金山天文台
2.Shanghai Academy of Spaceflight Technology
3.China Academy of Space Technology
First Author Affilication中国科学院紫金山天文台
Recommended Citation
GB/T 7714
Zhao Changyin,Zhang Wenxiang,Han Zengyao,et al. progressinspacedebrisresearch[J]. 空间科学学报,2010,30(5):516.
APA Zhao Changyin,Zhang Wenxiang,Han Zengyao,&Wang Hongbo.(2010).progressinspacedebrisresearch.空间科学学报,30(5),516.
MLA Zhao Changyin,et al."progressinspacedebrisresearch".空间科学学报 30.5(2010):516.
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