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: 2012-10-02
Time: 15:15
Room: TS02 (Sala Centauri, Hall 2)

IPC members

Chairman: Prof. Alessandro Francesconi, University of Padova - DII/CISAS, Italy;
Chairman: Mr. Martin Rudolph, Fraunhofer - Institute for High-Speed Dynamics, Germany;
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1		The Hypervelocity Impact Performance of Honeycomb Core Sandwich Panels	accepted	16'	withdrawn	Mr. Shannon Ryan	Defence Science and Technology Organisation (DSTO)	Australia
2		A Detailed Impact Risk Assessment Of Two Low Earth Orbiting Satellites	accepted	16'	confirmed	Dr. Hedley Stokes	PHS Space Ltd	United Kingdom
3		Debris Shielding for Inflatable Structures Development and Characterization at Hypervelocity Impacts	accepted	16'	withdrawn	Mr. Roberto Destefanis	Thales Alenia Space Italia	Italy
4		Terminal ballistics of flexible micrometeoroid and space debris protection shields	accepted	16'	confirmed	Mr. Martin Rudolph	Fraunhofer - Institute for High-Speed Dynamics	Germany
5		A model to describe the size distribution of satellite breakup debris	accepted	16'	confirmed	Mr. SHENGWEI LAN	China Aerodynamics Research and Development Center (CARDC)	China
6		Hyper Velocity Protection Developments on the Solar Probe Plus Mission	accepted	16'	confirmed	Mr. Douglas Mehoke	Johns Hopkins University Applied Physics Laboratory	United States
7		DESIGN AND FABRICATION OF DEBRISAT – A REPRESENTATIVE LEO SATELLITE FOR IMPROVEMENTS TO STANDARD SATELLITE BREAKUP MODELS	accepted	16'	confirmed	Dr. J.-C. Liou	National Aeronautics and Space Administration (NASA)	United States
8		Bulletproofing Satellites: Modeling the Physics of Hypervelocity Impacts	accepted	16'	withdrawn	Mr. Andrew Thurber	Virginia Tech	United States
9		Spacecraft Composite shielding system: Combination of normal and oblique bumpers	accepted	16'	withdrawn	Mr. Abrar-Ul-Haq Khan Baluch	Korea Advanced Institute of Science and Technology (KAIST)	Korea, Republic of
10		HVI-test Setup of in-situ Space Debris Detector	accepted	16'	confirmed	Mr. Waldemar Bauer	Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR)	Germany
11		Research of the space debris impact detecting system used on the space station	accepted	16'	no-show	Mr. Dongyong Jia	China Academy of Space Technology (CAST)	China
12		Preliminary Study on the test of the space small debris impact on solar cells	accepted	Poster	no-show	Mr. ruihai song		China
13		Hypervelocity Impact Experiment on Performance of Stuffed Whipple Shield with Al-mesh and Basalt Fiber Woven	accepted	Poster	no-show	Dr. Bin Jia	Harbin Institute of Technology	China
14		Research of Performance about Ceramic Coating on Aluminum Bumper to Resist Hypervelocity Impact	accepted	Poster	no-show	Dr. Gongshun Guan	Harbin Institute of Technology	China
15		Influence of multi-debris aerodynamic interactions during uncontrolled atmospheric reentry on the on-ground impact assessment	accepted	Poster	withdrawn	Mrs. Prevereaud Ysolde	ONERA	France
16		An Optimization Method of Ballistic Limit Equations via Correcting the Velocity Regions	accepted	Poster	withdrawn	Dr. Guanghui Jia	Beihang University	China
17		Pipes Vulnerability under MMOD Hypervelocity off-centered Impact	accepted	Poster	withdrawn	Dr. Guanghui Jia	Beihang University	China
18		An Investigation on Capability of Metal Mesh/Plate Multi-Shock Shield to Resist Hypervelocity Impact	accepted	Poster	no-show	Dr. Gongshun Guan	Harbin Institute of Technology	China