Proceedings Paper
Development tendency and key technology of deep space exploration's sample return capsule| Format | Member Price | Non-Member Price |
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Paper Abstract
As the key and fundamental technology of China Lunar Exploration Project, Sample Return Capsule will return to
earth from lunar for the first time. This paper introduces the contrast to typical foreign deep space Sample Return
Capsule's key performance such as Aerodynamic configuration, overload factor, entry range, stagnation point peak
heating base on investigating a great deal of typical deep space sample return missions. Finally, it gives the future
development direction of the deep space sample return mission, and offers some proposal for China Lunar
Exploration Project.
Paper Details
Date Published: 2 April 2010
PDF: 6 pages
Proc. SPIE 7651, International Conference on Space Information Technology 2009, 76510F (2 April 2010); doi: 10.1117/12.855776
Published in SPIE Proceedings Vol. 7651:
International Conference on Space Information Technology 2009
Xingrui Ma; Baohua Yang; Ming Li, Editor(s)
PDF: 6 pages
Proc. SPIE 7651, International Conference on Space Information Technology 2009, 76510F (2 April 2010); doi: 10.1117/12.855776
Show Author Affiliations
Zhuo-yi Xing, Beijing Institute of Spacecraft System Engineering (China)
Hui-guang Zhao, Beijing Institute of Spacecraft System Engineering (China)
Hui-guang Zhao, Beijing Institute of Spacecraft System Engineering (China)
Bo Wen, Beijing Institute of Spacecraft System Engineering (China)
Published in SPIE Proceedings Vol. 7651:
International Conference on Space Information Technology 2009
Xingrui Ma; Baohua Yang; Ming Li, Editor(s)
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