session 3

Title: Hypervelocity Impacts and Protection
Description: The session will address passive protection, shielding and damage predictions. Shielding aspects will be supported by experimental and computational results of HVI tests. Use of HVI techniques for debris mitigation.
Date: 2014-10-01
Time: 09:45
Room: 801B

IPC members

Co-Chair: Prof. Alessandro Francesconi, University of Padova - DII/CISAS, Italy;
Co-Chair: Dr. Sen Liu, China Aerodynamics Research and Development Center (CARDC) , China;
Rapporteur: Mr. Frank Schaefer, Fraunhofer - Institut für Kurzzeitdynamik, Ernst-Mach-Institut (EMI), Germany;

papers
Order	Time	Paper title	Selection result	Mode	Presentation status	Speaker	Affiliation	Country
1		MMOD Impact Damage to ISS	accepted	15'	withdrawn	Mr. James Hyde	Barrios Technology/ESC Group - NASA	United States
2		Measurement of micro-debris flux via TANPOPO capture panel onboard the ISS Kibo Exposed Facility	accepted	15'	confirmed	Ms. Yuu Takayanagi	Hosei University	Japan
3		influences of impact position and angle on shielding performance of n-shape configuration	accepted	15'	confirmed	Mr. Xuezhong Wen	China Aerodynamics Research and Development Center (CARDC)	China
4		hypervelocity impact characteristics of basalt fiber woven/al-mesh combination bumper stuffed in whipple shield	accepted	15'	withdrawn	Dr. Bin Jia	Harbin Institute of Technology	China
5		An engineering model to describe fragments clouds propagating inside spacecraft in consequence of space debris impact on sandwich panel structures	accepted	15'	confirmed	Prof. Alessandro Francesconi	University of Padova - DII/CISAS	Italy
6		Determination of coordinates for a point of pressurized compartment puncture at collision with a high-speed particle	accepted	15'	withdrawn	Dr. Vladimir Lapygin	Central Research Institute for Machine Building (JSC TSNIIMASH)	Russian Federation
7		EXPERIMENTAL VERIFICATION OF AN INNOVATIVE DEBRIS DETECTOR	accepted	15'	confirmed	Mr. Waldemar Bauer	Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR)	Germany
8		The study of small space debris impact inducing discharge	accepted	15'	withdrawn	Dr. Li Hongwei	National Space Science Center (NSSC), Chinese Academy of Sciences	China
9		Modeling of damage formation on a front wall of shielded composite overwrapped pressure vessel subjected to space debris impact	accepted	15'	confirmed	Prof. Igor Telichev	University of Manitoba	Canada
10		Multi-shock shield performance at 15 MJ for catalogued debris	accepted	15'	withdrawn	Dr. Joshua Miller	National Aeronautics and Space Administration (NASA), Johnson Space Center	United States
11		cardc-sbm spacecraft breakup model and its application	accepted	15'	confirmed	Dr. Sen Liu	China Aerodynamics Research and Development Center (CARDC)	China
12		A new method to predict the catastrophic disintegration of spacecraft upon collision with large orbital debris	accepted	15'	confirmed	Dr. Mirco Zaccariotto	University of Padova, DII / CISAS – “G. Colombo”	Italy