session 3

Title: Hypervelocity Impacts and Protection
type: oral
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: 2016-09-28
Time: 09:45
Room: Salon Jalisco E7

IPC members

Co-Chair: Dr. Norman Fitz-Coy, University of Florida, United States;
Rapporteur: Mr. Frank Schaefer, Fraunhofer - Institut für Kurzzeitdynamik, Ernst-Mach-Institut (EMI), Germany;

papers
Order	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	A Vulnerability Analysis Method of Spacecraft under Space Debris Impact	18'	withdrawn	Dr. Sen Liu	China Aerodynamics Research and Development Center (CARDC)	China
2	Influence on Shielding performance of aerogel/fiberglass composite stuffed in shield	18'	withdrawn	Mr. Xuezhong Wen	China Aerodynamics Research and Development Center (CARDC)	China
3	A Study of Damage on Woven Multi-Shock Shield by a High-Speed Impact of Aluminum Sphere at Different Ambient Temperature	18'		Dr. Gongshun Guan	Harbin Institute of Technology	China
4	Experimental study of the Cryogenic Effect on Hypervelocity Impact Characteristics of Aluminum Alloy Whipple Structure	18'	confirmed	Prof. Zizheng GONG	China Academy of Space Technology (CAST)	China
5	An Update on DebriSat's Debris Categorization System	18'	confirmed	Mr. Joe Kleespies	University of Florida	United States
6	Size Characterization using a Two-Dimensional Approximation for DebriSat Fragments	18'	confirmed	Mr. Matthew Moraguez	University of Florida	United States
7	MICROMETEOROID AND ORBITAL DEBRIS IMPACT HARDNESS ASSURANCE OF AN ORBITAL SPACEPLANE	18'	confirmed	Mr. Anton Nikiforov	Yuzhnoye State Design Office	Ukraine