IAF Digital Library

3

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: 2017-09-27
Time: 09:45
Room: Hall E1

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		Review of MMOD Shielding of the Chinese Space Station	18	confirmed	Dr. Jun Yan	China Academy of Space Technology (CAST)	China
2		Predicting the Consequences of Micrometeoroid and Orbital Debris Penetrations on the International Space Station	18	withdrawn	Mr. James Hyde	Barrios Technology/ESC Group - NASA	United States
3		hypervelocity impact damage pattern recognition in aluminum alloy plates based on d-s evidence theory and bp neural network	18		Dr. cao wuxiong	School of Astronautics, Harbin Institute of Technology	China
4		Study on the performance of shielding configuration for reducing the fixing weight of fiber layer	18	confirmed	Mr. Fa-wei Ke	China Aerodynamics Research and Development Center (CARDC)	China
5		The influence of mechanical laminate properties on the hypervelocity impact resistance of Fiber Metal Laminates	18	withdrawn	Mr. Chunsen Shi	Delft University of Technology (TU Delft)	The Netherlands
6		Characterizing DebriSat Fragments: So many fragments, so much data, and so little time	18	confirmed	Mr. Bungo Shiotani	University of Florida	United States
7		Optical Fragment Tracking in Hypervelocity Impact Experiments	18	confirmed	Mr. Erkai Watson	Fraunhofer - Institut für Kurzzeitdynamik, Ernst-Mach-Institut (EMI)	Germany
8		Experimental investigation on the damage characteristic of solar array under millimeter size orbital debris hypervelocity impact	18	confirmed	Prof. Zizheng GONG	Beijing Institute of Spacecraft Environment Engineering, China Academy of Space Technology (CAST)	China
9		Microwave Emission from Hypervelocity Impacts Using Aluminum and Nylon for Target and Projectile Materials	18	confirmed
10		Spacecraft Debris Generation due to Materials Degradation for LEO Orbit Conditions	18	withdrawn	Mr. Paulo Gordo	Faculdade de Ciências da Universidade de Lisboa	Portugal
–		Risk assessment of sustained discharge on satellite’s power harnesses caused by space debris impacts		withdrawn	Dr. Takayuki Hirai	Japan Aerospace Exploration Agency (JAXA)	Japan