MENG Linzhi, DONG Jie, XU Yingqiao, WANG Shuo. Analysis of Key Technologies for Unmanned Mars Sample Return Mission[J]. Journal of Deep Space Exploration, 2016, 3(2): 114-120,128. doi: 10.15982/j.issn.2095-7777.2016.02.003
| Citation: |
MENG Linzhi, DONG Jie, XU Yingqiao, WANG Shuo. Analysis of Key Technologies for Unmanned Mars Sample Return Mission[J].Journal of Deep Space Exploration, 2016, 3(2): 114-120,128.doi:10.15982/j.issn.2095-7777.2016.02.003
|
Analysis of Key Technologies for Unmanned Mars Sample Return Mission
- 1.
Beijing Institute of Spacecraft System Engineering, Beijing 100094, China
- 2.
China Academy of Technology Beijing 100094, China
- Received Date:2016-03-05
- Rev Recd Date:2016-04-06
Abstract
Unmanned Mars sample return mission is of great significance to obtain scientific results and improve engineering ability. The mission period is longer and technical risk is higher compared with several foreign Mars landing and roving missions. The top-level system design is determined by the mission flight mode. The rendezvous capture and sample transfer process should be completed near the Mars orbit. Therefore, two probes with different functions are required:one is used to perform Mars capture, sample storage and Mars-Earth transfer, the other to complete EDL process, Mars surface ascent and sample delivery. Such key issues as EDL mode, Mars ascent vehicle, Mars orbit rendezvous and capture, sample transfer, earth entry vehicle, system scales, rocket selection, etc. are analyzed in this paper. The main technical difficulty and solution approaches are discussed.
References
| [1] |
Beaty D W,Grady M,Moura D,et al. Preliminary planning for an international Mars sample return mssioin:report of the international Mars architecture for the return of samples (iMARS)working group[J]. Journal of Henan Judicial Police Vocational College,2014.
|
| [2] |
Wercinski P F. Mars sample return:a direct and minimum-risk design[J]. Journal of Spacecraft and Rockets,1996,33(3):381-385.
|
| [3] |
Fujita K,Ozawa T,Okudaira K,et al. Conceptual study and key technology development for Mars aeroflyby sample collection[J]. Acta Astronautica,2014(93):84-93.
|
| [4] |
Gardini B. The aurora Mars sample return mission[C]//The 54th International Astronautical Congress of the International Astronautical Federation,the International Academy of Astronautics,and the International Institute of Space Law. Bremen,Germany:IAC,2003.
|
| [5] |
Richard Mattingly. Mars sample return as a campaign[C]//IEEE Aerospace Conference. California Institute of Technology:Jet Propulsion Laborator,2011:1-13.
|
| [6] |
杨孟飞,张高,张伍,等. 探月三期月地高速再入返回飞行器技术设计与实现[J]. 中国科学:技术科学,2015,45(2):111-123.Yang M F,Zhang G,Zhang W,et al. Technique design and realization of the circumlunar return and reentry spacecraft of 3rd phase of Chinese lunar exploration program[J]. Science China Technological Sciences,2015,45(2):111-123.
|
| [7] |
Benton M,Segundo E L,Bamford R. Concept for human exploration of neo asteroids using mpcv,deep space vehicle,artificial gravity module,and mini-magnetosphere radiation shield[C]//The 44th AIAA SPACE 2011 Conference and Exposition. Long Beach,CA:AIAA,2011,1-45.
|
| [8] |
耿云飞,高洁,陆亚东,等. 轻小型再入飞行器发展研究[J]. 航天器工程,2014,23(6):99-104.Geng Y F,Gao J,Lu Y D,et al. Demonstration of light reentry vehicle development[J]. Spacecraft Engineering,2014,23(6):99-104.
|
| [9] |
Samareh J,Glaab L,Winski R G,et al. Multi-mission system analysis for planetary entry (M-SAPE)Version 1.[EB/OL]. (2016-03-25)[2016-03-25]. http://www.ntrs.nasa.gov.
|
Proportional views
-
DownLoad: