session 2

Title

Space Structures II - Development and Verification (Deployable and Dimensionally Stable Structures)

Description

The topics to be addressed include evaluation of analysis versus test results for deployable and dimensionally stable structures, e.g. reflectors, telescopes, antennas; examination of both on-ground and in-orbit testing, thermal distortion and shape control, structural design, development and verification; lessons learned.

Date

2013-09-24

Time

09:45

Room

306B

IPC members
papers

Order

Time

Paper title

Selection result

Mode

Presentation status

Speaker

Affiliation

Country

1

KEYNOTE LECTURE: Space Structure – Yesterday, Today and Tomorrow

accepted

30'

confirmed

Prof. Tetsuo Yasaka

QPS Institute

Japan

2

A New Approach to Stabilization of Inflatable Space Structures

accepted

15'

confirmed

Mr. Manpreet Puri

University of Strathclyde

United Kingdom

3

On-orbit experimental results of the REX-J extendable robotic manipulator

accepted

15'

confirmed

Mr. Atsushi Ueta

Japan Aerospace Exploration Agency (JAXA)

Japan

4

Characterizing Lightweight and Dimensionally Ultra Stable Structures for Space Application

accepted

15'

confirmed

Mr. Ruven Spannagel

DLR, German Aerospace Center

Germany

5

Thermal property and microstructure contrast of three kinds of carbon/silicon carbide composites

accepted

15'

withdrawn

Dr. Jin Li

China Aerospace Science and Technology Corporation (CASC)

China

6

Deployment analysis and control strategies of flexible space manipulators

accepted

15'

confirmed

Mr. Andrea Pisculli

University of Rome "La Sapienza"

Italy

7

Multibody analysis of a two axis oriented deployable Solar Array

accepted

15'

withdrawn

Mrs. Anne GIOVANNINI

Thales Alenia Space France

France

8

Design and evaluation of inflatable structural concepts for aerodynamic drag augmentation.

accepted

15'

confirmed

Mr. Gabriel Secheli

Surrey Space Centre, University of Surrey

United Kingdom

9

Shape Measurement of Creased Large Space Membrane by Photometric Stereo Technique

accepted

15'

confirmed

Prof. Hiroshi Furuya

Tokyo Institute of Technology

Japan

10

Equivalent Stiffness of Large Deployable Membrane with Random Initial Deformation

accepted

15'

confirmed

Ms. Ayumu Yamasaki

Tokyo Institute of Technology

Japan

11

Parametric Study of Flexible Solar Array Based on Orthogonal Method

accepted

15'

confirmed

Dr. Liu Dali

Aerospace System Engineering Shanghai

China

12

Minimum Weight Design of Orthotropic Cylindrical Launcher Shell Structures subjected to Local Load Introduction

accepted

15'

confirmed

Dr. Jochen Albus

Airbus DS GmbH

Germany

NUMERICAL SIMULATION OF FOLDING AND DEPLOYING PROCESS OF LENTICULAR COLLAPSIBLE COMPOSITE BOOMS

merged with 17932

Dr. Guangqiang Fang

Aerospace System Engineering Shanghai

China