session 6

Title: Space Environmental Effects and Spacecraft Protection
Description: The focus of the session will be on space environmental effects and spacecraft protection. The effects of vacuum, radiation, atomic oxygen, spacecraft charging, thermal cycling, dissociation, meteoroids and space debris impact on space systems, materials and structures, and microelectronics will be addressed. Protective and shielding technologies, including analysis simulation and testing of debris impact, and susceptibility of Commercial-Off-The-Shelf (COTS) micro-electronics to space radiation will be covered.
Date: 2013-09-26
Time: 09:45
Room: 306B

IPC members

Co-Chair: Dr. Giuliano Marino, CIRA Italian Aerospace Research Centre, Italy;
Co-Chair: Dr. Iuriy Moshnenko, Yuzhnoye State Design Office, Ukraine;
Rapporteur: Prof. Franz-Josef Kahlen, University of Cape Town, South Africa;

papers
Order	Paper title	Selection result	Mode	Presentation status	Speaker	Affiliation	Country
1	Ground thermal radiation vacuum tests and thermal-structural analysis for thin-walled CFRP lenticular cross-section space boom	accepted	15'		Prof. Chen Wujun	Space Structures Research Center, Shanghai Jiao Tong University	China
2	protection of spacecraft from space environmental effects	accepted	15'	confirmed	Mr. Srikanth Raviprasad	Manipal Institute of Technology, Manipal University	India
3	Aerobraking effects induced erosion of Kapton	accepted	15'		Mr. Hu Longfei	China Academy of Aerospace Aerodynamics (CAAA)	China
4	analytical study of thermal and mechanical properties of syntactic foams for space applications	accepted	15'	confirmed	Mr. Anthony Kulesa	South Dakota School of Mines and Technology	United States
5	Thermal shielding of a sphere-cone reentry vehicle	accepted	15'	confirmed	Dr. Xiaoyan Li	Research & Development Center of China Academy of Vehicle Technology	China
6	RADIATION SHIELDING AGAINST SPES AND GCRS WITH PLASMA INDUCED MAGNETIC FIELDS	accepted	15'	withdrawn	Ms. Emmanuelle Dujols	Propulsion and Research Center	United States
7	Contamination Measurement and Control of Chinese Spacecraft	accepted	15'	confirmed	Dr. Yang Dongsheng	China Academy of Space Technology (CAST)	China
8	The temperature dependence of solar sail materials on a heliocentric distance	accepted	15'	confirmed	Prof. Roman Ya. Kezerashvili	New York City College of Technology	United States
9	ANALYSIS OF COMPOSITE PLATE SUBJECT TO SPACE DEBRIS IMPACT FOR UNLIKELY PENETRATION CASE	accepted	15'	confirmed	Prof. Harijono Djojodihardjo	Universitas Al Azhar Indonesia	Indonesia
10	Aerothermodynamics of a reentry vehicle nose with a forward facing conical cavity	accepted	15'		Mr. Rajesh Yadav	University of Petroleum and Energy Studies	India
11	thermal-structural analysis of solar cells on flexible solar array	accepted	15'		Ms. Yuhan Zhang	School of Aerospace and Mechanics, Tongji University	China
12	the appropriate technique for the microsatellite hardware design in line with the reduction cost: mitigation the radiation effects over a micro satellite flying in low equator orbit	accepted	15'	withdrawn	Mr. Bustanul Arifin	Indonesian National Institute of Aeronautics and Space (LAPAN)	Indonesia
13	Hardness Assurance Evaluation of Microcontrollers for Satellite Electronics with Laser pulses	accepted	10'	confirmed	Ms. vafa sedghi		Iran

session 6

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