PDF(2178 KB)
Topic:Deep Space Extreme Environment Protection and New Materials
Topic:Deep Space Extreme Environment Protection and New Materials
Performance Analysis and Experimental Study of Tianwen-1 Parachute Material
- HUANG Mingxing, GAO Shuyi, WANG Liwu, WANG Wenqiang, LI Jian
Author information
+
Beijing Institute of Space Mechanics and Electricity, Beijing 100094, China
Show less
History
+
Received |
Revised |
Published |
11 Apr 2021 |
14 Jul 2021 |
20 Oct 2021 |
Issue Date |
|
20 Oct 2021 |
|
{{custom_sec.title}}
{{custom_sec.title}}
{{custom_sec.content}}
This is a preview of subscription content, contact
us for subscripton.
References
[1] HUSSONG J, LAU R. The Viking Mars lander decelerator system[C]//3th Aerodynamic Deceleration Systems Conference. Dayton, OH, USA: AIAA, 1970.
[2] WITKOWSKI A. Mars pathfinder parachute system performance[C]//15th Aerodynamic Decelerator Systems Technology Conference. Toulouse, France: AIAA, 1999.
[3] WITKOWSKI A, BRUNO R. Mars exploration rover parachute decelerator system program overview[C]//17th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar. Monterey, California: AIAA, 2003.
[4] SENGUPTA A, WITKOWSKI A, ROWAN J, et al. Overview of the Mars science laboratory parachute decelerator system[C]//19th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar. Williamsburg, VA: AIAA, 2007.
[5] GROVER M R, CICHY B D, DESAI P N. Overview of the phoenix entry, descent, and landing system architecture[J]. Journal of Spacecraft and Rockets,2011,48(5):706-712
[6] UNDERWOOD J, BOWN N. An entry, descent and landing system for the beagle2 Mars mission[C]//16th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar. Boston, MA, USA: AIAA, 2001.
[7] 饶炜, 孙泽洲, 孟林智, 等. 火星着陆探测任务关键环节技术途径分析[J]. 深空探测学报(中英文),2016,3(2):121-128
RAO W, SUN Z Z, MENG L Z, et al. Analysis and design for the Mars entry, descent and landing mission[J]. Journal of Deep Space Exploration,2016,3(2):121-128
[8] KNACKE T W. Parachute recovery systems design manual[M]. Santa Barbara : CA, Para Publishing, 1992.
[9] 高树义, 戈嗣诚, 梁艳. 火星盘缝带伞跨声速风洞试验研究[J]. 中国空间科学技术,2015(4):69-75
GAO S Y, GE S C, LIANG Y. Research on transonic wind tunnel tests of Mars disk-gap-band parachutes[J]. Chinese Space Science and Technology,2015(4):69-75
[10] 耿言, 周继时, 李莎, 等. 我国首次火星探测任务[J]. 深空探测学报(中英文), 2018, 5(5): 399-405.
GENG Y, ZHOU J S, LI S, et al. A brief introduction of the first Mars exploration mission in China[J]. Journal of Deep Space Exploration, 2018, 5(5): 399-405.
[11] ECKSTROM C V. Development and testing of the disk-gap-band parachute used for low dynamic pressure applications at ejection altitudes at or above 200, 000 feet[R]. USA: NASA, 1966.
[12] ECKSTROM C, MURROW H. Description of a new parachute designed for use with meteorological rockets and a consideration of improvements in meteorological measurements[C]//Conference on Aerospace Meteorology. Los Angeles, CA, USA: AIAA, 1966.
[13] 黄明星, 王文强, 李健, 等. 基于有效透气量对火星降落伞气动力系数预测分析[J]. 宇航学报, 2020, 41(9): 1132-1140.
HUANG M X, WANG W Q, LI J, et al. Prediction and analysis of aerodynamic coefficient of parachute under Mars conditions based on effective porosity[J].Journal of Astronautics, 2020, 41(9): 1132-1140.
[14] KNACKE T. Parachute recovery systems design manual[M]. USA, China Lake: Recovery Systems Division Aerosystems Departement, 1991.
[15] 姚穆. 纺织材料学[M]. 北京: 中国纺织出版社, 2015.
[16] FALLON I E. System design overview of the Mars pathfinder parachute decelerator subsystem[C]//14th Aerodynamic Decelerator Systems Technology Conference. USA: AIAA, 1997.
[17] WITKOWSKI A. Mars scout phoenix parachute decelerator system program overview[C]//2007 IEEE Aerospace Conference. Big Sky, MT, USA: IEEE, 2007.
[18] SENGUPTA A, STELTZNER A, WITKOWSKI A, et al. An overview of the mars science laboratory parachute decelerator system[C]//2007 IEEE Aerospace Conference. Big Sky, MT, USA: IEEE, 2007.
[19] WITKOWSKI A, KANDIS M, KIPP D, et al. Mars insight parachute system performance[C]//AIAA Aviation 2019 Forum. Dallas, Texas: AIAA, 2019.
[20] TUTT B A, LOWRY C W, CLARK I G, et al. Design overview of the strengthened Mars 2020 parachute assembly[C]//AIAA Aviation 2019 Forum. Dallas, Texas: AIAA, 2019.