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: 2011-10-05
Time: 15:00
Room: TS-15

IPC members

Chairman: Dr. Sergey Meshcheryakov, TSNIIMASH, Russian Federation;
Chairman: Dr. Frank Schäfer, Fraunhofer EMI, Germany;
Rapporteur: Mr. James Hyde, Barrios Technology/ESC Group - NASA, United States;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1		Hypervelocity Impact Testing of Advanced Materials and Structures for Micrometeoroid and Orbital Debris Shielding	15	confirmed	Dr. Shannon Ryan	Defence Science and Technology Organisation (DSTO)	Australia
2		Verification on hypervelocity impact tests of ejecta and data analysis of witness plates after the impact tests	15	confirmed	Prof.Dr. Yasuhiro Akahoshi	Kyushu Institute of Technology	Japan
3		Interpretation of impact features on the surface of the WFPC-2 radiator	15	withdrawn	Dr. Phillip Anz-Meador	ESCG/Jacobs	United States
4		Electrical response of current-carrying space-grade harnesses to hypervelocity impact	15	confirmed	Mr. Martin Rudolph	Fraunhofer EMI	Germany
5		Electrical breakdowns on SC surfaces due to microparticles impacts	15	withdrawn	Dr. Sergey Meshcheryakov	TSNIIMASH	Russian Federation
6		Electrical Effects of Hypervelocity Impacts	15	confirmed	Mr. Ashish Goel	Stanford University	United States
7		Shuttle Hypervelocity Impact Database	15	confirmed	Mr. James Hyde	Barrios Technology/ESC Group - NASA	United States
8		Fragment Characteristic of Simulated Spacecraft under Hypervelocity Impact	15	confirmed	Mr. SHENGWEI LAN	China Aerodynamics Research and Development Center (CARDC)	China
9		Improvements for Space Mission Protection against Space-Debris Hazards	15	confirmed	Mr. Jeffrey Apeldoorn	OHB System AG	Germany
10		Computational Methodology to Predict Satellite System-level Effects from Untrackable Space Debris	15	confirmed	Mr. Nathan Welty	Fraunhofer EMI	Germany
11		DEVELOPMENT OF IN-SITU MICRO-DEBRIS MEASUREMENT SYSTEM	15	confirmed	Dr. Yukihito Kitazawa	IHI Corporation	Japan
12		Development of an implosion-driven hypervelocity launcher for orbital debris and micrometeoroid simulation	15	confirmed	Mr. Justin Huneault	McGill University	Canada
21		SHIELDED AND UNSHIELDED LOOP HEAT PIPE IN SPACECRAFT TO HYPERVELOCITY IMPACTS	15'	confirmed	Ms. Yuhua Huo	China Academy of Space Technology (CAST)	China