IAF Digital Library

3

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: 2015-10-14
Time: 09:45
Room: Eshkol 2 (ICC, lower level)

IPC members

Co-Chair: Mr. Frank Schaefer, Fraunhofer - Institut für Kurzzeitdynamik, Ernst-Mach-Institut (EMI), Germany;
Co-Chair: Dr. Norman Fitz-Coy, University of Florida, United States;
Rapporteur: Prof. Alessandro Francesconi, University of Padova - DII/CISAS, Italy;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1		A new Ballistic Limit Equation for thin tape tethers	18'	confirmed	Prof. Alessandro Francesconi	University of Padova - DII/CISAS	Italy
2		Experimental and Numerical Investigations of Stuffed Whipple Shields Protecting Chinese Manned Spacecraft against Orbital Debris	18'	confirmed	Dr. Li Shan	Institute of Spacecraft System Engineering,China Academy of Space Technology (CAST)	China
3		preliminary study on the performance of shielding configuration with stuffed layer under hypervelocity impact	18'	confirmed	Mr. Fa-wei Ke	China Aerodynamics Research and Development Center (CARDC)	China
4		Simplified S/C vulnerability assessments at component level in early design phase at ESA’s CDF	18'	confirmed	Mr. Scott Kempf	Fraunhofer - Institut für Kurzzeitdynamik, Ernst-Mach-Institut (EMI)	Germany
5		Electrical Phenomena caused by Hypervelocity Impact	18'	confirmed	Dr. Tanaka Koji	ISAS/JAXA	Japan
6		Integration of a Dust Accelerator into the IPG6-B Facility for Material Impact Tests	18'	confirmed	Mr. Christoph Montag	Institute of Space Systems, University of Stuttgart	Germany
8		experimental study for Laser-driven flyer plates up to 8 km/s	18'	confirmed	Prof.Dr. Zizheng GONG	China Academy of Space Technology (CAST)	China
9		mass distribution and dependence on impact parameters of spacecraft breakup debris	18'	confirmed	Mr. SHENGWEI LAN	China Aerodynamics Research and Development Center (CARDC)	China
10		Hyper velocity impact analysis of cube sat and subsequent orbit determination	18'	withdrawn	Dr. Ugur Guven		United States
–		recent progresses of micro-space debris hypervelocity impact tests using laser-driven flyer techniques in CAST	MERGED 29049	confirmed	Prof.Dr. Zizheng GONG	China Academy of Space Technology (CAST)	China