空间探测烧蚀防热材料应用及发展

doi:10.11896/cldb.22040315

Abstract
Figure/Table
References
Related Citation (9)

Download:

Full Text ( PDF ) (7334KB)
Export: BibTeX | EndNote (RIS)

Abstract Ablation thermal protection materials are used for the most of space probes due to high reliability and wide suitability. Ablation thermal protection materials have various kinds for defferent space exploration goals, entry/reentry trajactory of probe, probe configuration and limit of thermal protection strcture. Light and efficient are the important development characteristic of the ablation thermal protection materials. Furthermore, the reliability is vital important. Different thermal protection materials have different behaviors and characteristics in the different heat environment. Ablation thermal protection materials have critical role for the success of space exploration. The kinds and applications of ablation thermal protection materials for space exploration have been reviewed, including high density glass fiber reinforced phenolic plastics, honeycomb reinforced thermal protection material, resin infiltrated materials, carbon phenolic of US, and nylon phenolic, honeycomb reinforced thermal protection materials and NF materials of China. The applied space exploration probe, aerodynamic heating environment, the material properties and manufacture technology of the thermal protection structure are introduced. The anomaly ablation cases of the materials and the selected materials change of US space exploration are summarized. It is thus clear that the coupling relationship between thermal protection material and heat environment is complex. The research of thermal protection material on resisting anomaly damage in US and our country are introduced. It is showed that the honeycomb reinforced ablation thermal protection materials has advantages for the existing experiment results. The application and development of the thermal protection materials for space exploration are prospected at the end.

Key words： space exploration ablation thermal protection structure

Published: 25 November 2022 Online: 2022-11-25

CLC number:

TB33

	Service
	E-mail this article
	Add to my bookshelf
	Add to citation manager
	E-mail Alert
	RSS
	Articles by authors
	LIANG Xin
	SONG Zhaohui
	FANG Zhou
	DENG Huoying
	MAO Kezhu
	WU Dongri

Cite this article:

LIANG Xin,SONG Zhaohui,FANG Zhou, et al. Application and Trend of Ablation Thermal Protection Materials for Space Exploration[J]. Materials Reports, 2022, 36(22): 22040315-8.

URL:

http://www.mater-rep.com/EN/10.11896/cldb.22040315 OR http://www.mater-rep.com/EN/Y2022/V36/I22/22040315

1 John H B, Kenneth S K. In: AlAA 61h Annual Meeting and Technical DisDlay.Anaheim, California, 1969.
2 Donald M C. Thermal protection systems manned spacecraft flight expe-rience. N93-12449, NASA,1992.
3 Bryanerb R, Greenshields D H, Chauvin T, et al. Journal of Spacecraft and Rockets, 1970, 7(6), 727
4 Graves R A,Wittte W G. Flight-test analysis of Apollo heat-shield mate-rial using the pacemaker vehicle system. NASA-TN-D-4713, 1968.
5 Acrouch R K, Walberg G D. Investigation of ablation behavior of Avcoat 5026 39M over a wide range of thermal environment. NASA-TM-X-1778 69N22933, 1969.
6 Richard A T, Victor L, Thomas J, et al. In: 47th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. Orlando, Florida, 2009.
7 Brian R H, Karen T B, Thomas J H. In: 46^th AIAA Aerospace Sciences Meeting and Exhibit. Reno, Nevada, 2008.
8 Brian R H, Thomas J H, Karen T B, et al. Experimental investigation of project orion crew exploration vehicle aeroheating in AEDC Tunnel 9. NASA/TP -2008-215547. Hampton, Virginia: NASA, 2008.
9 John K. In: 7^th International Planetary Probe Workshop.Barcelona, Spain, 2010.
10 Willcockson H W. Journal of Spacecraft and Rockets,1999, 36(3),374.
11 Adam S, Prasun D, Wayne L, et al. In: AIAA ADS Conference. Monterey, California, 2003.
12 Michael J W, Chun Y T,Karl T E, et al. In: 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. Orlando, Florida, 2010.
13 Huy T, Michael T, William H, et al. Ames research center shear tests of SLA-561V heat shield material for Mars-Pathfinder. NASA-TM-110402 96N34006, NASA, 1996.
14 Hollis B R, Liechty D S. Journal of Spacecraft and Rockets,2006, 43(2),354.
15 Mckinney J, Ferguson P,Weber M L, et al. Boeing CST-100 landing and recovery system design and development testing, AIAA-2013-1262. Reston: AIAA,2013
16 Richard A T, Victor L, Thomas J, et al. In: 47th AIAA Aerospace Sciences Meeting Including The New Horizons Forum and Aerospace Exposition. Orlando, Florida, 2009.
17 Brian R H, Karen T B, Thomas J H. In: 46^th AIAA Aerospace Sciences Meeting and Exhibit. Reno, Nevada, 2008.
18 Brian R H, Thomas J H, Karen T B, et al. Experimental Investigation of Project Orion Crew Exploration Vehicle Aeroheating in AEDC Tunnel 9. NASA/TP-2008-215547. Hampton, Virginia: NASA, 2008.
19 Ethiraj V, James R. In: 6^th International Planetary Probe Workshop, 2008.
20 Robin A S B, David M D, Eric M S. In: 6^th International Planetary Probe Workshop.Atlanta, Georgia,USA, 2008.
21 Beck R, Driver D, Wright M, et al. In: 41^st AIAA Thermophysics Conference. San Antonio, TX, 2009.
22 Beck R, Driver D, Wright M, et al. In: AIAA-2009-4229, 41^st AIAA Thermophysics Conference. San Antonio, Texas, 2009.
23 Huy K T, Christine E J, Daniel J R, et al. Phenolic impregnated carbon ablators (PICA) as thermal protection systems for discovery missions. NASA-TM-110440 97N19369, NASA,1997.
24 Edquist K T, Hollis B R, Dyakonov A A. Mars science laboratory entry capsule aerothermo-dynamics and thermal protection system. In: NASA IEEAC Paper 1423, 2007.
25 White T, Hwang H, Ellerby D. Thermal Protection System Materials for Sample Return Missions. The NRC Decadal Survey Sub-Panels,2020.
26 Ellerby D. In: The 10th Ablation Workshop. Burlington, VT, 2018.
27 Milos F S, Chen Y K, Squire T H, et al. Journal of Spacecraft and Roc-kets,1999, 36(3),298.
28 Fimmel R O, Colin L, Burgess E.Pioneer Venus.NAS 1.21:461; NASA-SP-461, 83N30340, NASA,1983.
29 Willcockson B. Genesis sample return capsule overview. NASA-20070014646, NASA, 2005.
30 Laub B, Chen Y K.In: 41st AIAA Thermophysics Conference. San Antonio, TX, 2009.
31 Jean-Marc B, Francine B, Ludovic D, et al.In: 4th International Planetary Probe Workshop. Pasadena,California, 2006.
32 Karl T E, Artem A D,Michael J, et al.In: 41st AIAA Thermophysics Conference. San Antonio, Texas, 2009.
33 Ethiraj V, James R. In: 6th International Planetary Probe Workshop.Atlanta, Georgia,USA, 2008.
34 Kowal T J.In: JSC Commercial Human Space Flight Symposium.Houston, TX, 2010.
35 Jiang G Q. Chinese Space Science and Technology,1990(6),34(in Chinese).
姜贵庆.中国空间科学技术,1990(6),34
36 Xing L Q. Chinese Space Science and Technology,1991(2), 26(in Chinese).
邢连群.中国空间科学技术,1991(2),26.
37 Wang C M, Liang X, Sun B G, et al. Aerospace Materials & Technology, 2011, 41(2), 6(in Chinese).
王春明,梁馨,孙宝岗,等.宇航材料工艺,2011, 41(2), 6.
38 Dong Y Z, Liu F, Yang C H, et al. Scientia Sinica(Technologica), 2015, 45(2), 151(in Chinese).
董彦芝,刘峰,杨昌昊,等.中国科学:技术科学, 2015,45(2),151.
39 Zhang X, Dong W, Ma N, et al.Spacecraft Environment Engineering, 2018, 35(6), 599(in Chinese).
张璇,董薇,马宁,等.航天器环境工程,2018, 35(6),599.
40 Ethiraj V. In: 10th Ablation Workshop. Burlington,VT, 2018.