session 6

Title

Space Environmental Effects and Spacecraft Protection

Description

The focus of the session will be on space environmental effects and spacecraft protection. The effects of vacuum, radiation, atomic oxygen, spacecraft charging, thermal cycling, dissociation, meteoroids and space debris impact on space systems, materials and structures, and microelectronics will be addressed. Protective and shielding technologies, including analysis simulation and testing of debris impact, and susceptibility of Commercial-Off-The-Shelf (COTS) micro-electronics to space radiation will be covered.

Date

2014-10-02

Time

09:45

Room

713A

IPC members
papers

Order

Time

Paper title

Selection result

Mode

Presentation status

Speaker

Affiliation

Country

1

dust cleaning, transportation and sampling in lunar environment using traveling electric field

accepted

12'

confirmed

Mr. Nima Gharib

McGill University

Canada

2

Predicting Erosive Wear by Exhaust-Blown Lunar Dust through Experimentally-Validated Computational Modeling

accepted

12'

confirmed

Dr. Jeremiah Mpagazehe

Carnegie Mellon University

United States

3

Cubesat in-situ degradation detector (CIDD)

accepted

12'

confirmed

Dr. Benny Rievers

ZARM University of Bremen

Germany

4

A solar sail coated by materials that undergo desorption for a space exploration

accepted

12'

confirmed

Prof. Roman Ya. Kezerashvili

New York City College of Technology

United States

5

high velocity impact behavior of composite sandwich panels with self-healing capabilities

accepted

12'

confirmed

Mr. Teo Mudric

CISAS – “G. Colombo” Center of Studies and Activities for Space, University of Padova

Italy

6

Effects of Thermal Cycling on Mechanical and Physical Properties of High Performance Carbon/Epoxy Composites Applied to Satellite Antenna

accepted

12'

confirmed

Mr. Han Jianping

Xi’an Aerospace Composite Materials Institute

China

7

Total Electron Emission Yield Measurement of Insulating Materials Due to Different Temperatures

accepted

12'

confirmed

Mr. Akira Miayahra

Kyushu Institute of Technology

Japan

8

Characteristic measurements and tests of newly lightweight Mg-Li alloys

accepted

12'

withdrawn

Dr. Fei Zhou

Shanghai Institute of Satellite Engineering

China

9

numerical simulation of delaminations induced by drop-weight impact in composite space structures and correlation with experiments

accepted

12'

confirmed

Dr. Davide Nardi

University of Rome "La Sapienza"

Italy

10

Finite Element Computational Modeling and Simulation Studies of Space Debris Non-Penetrating Impact on Space Structure

accepted

12'

confirmed

Prof. Harijono Djojodihardjo

Universitas Al Azhar Indonesia

Indonesia

11

The Study of Internal Charging and Discharging Effects on Solar Array Drive Mechanism

accepted

12'

confirmed

Dr. Rui Li

Beijing Institute of Control Engineering, China Academy of Space Technology (CAST)

China

12

Low Cost Thermal-Vacuum System for the Development of Very Small Spacecraft

accepted

12'

confirmed

Dr. Tatsuo Shimizu

Kyushu Institute of Technology

Japan

13

The laboratory calibration of a novel surface potential monitor at GEO

accepted

12'

no-show

Dr. chaoyang zhou

Lanzhou Institute of Physics

China

14

Application of TMR method to On-board control unit

accepted

12'

no-show

Mr. KWON RYONG

Korea, Democratic People's Republic of