session 1

Title

Space Structures I - Development and Verification (Space Vehicles and Components)

Description

The topics to be addressed include evaluation of analysis versus test results, spacecraft and launch vehicles system and subsystems, e.g. pressurised structures, tanks, loads introduction, primary structures, fluidic equipment, control surfaces; examination of both on-ground and in-orbit testing, launch dynamic environment as related to structural design, space vehicles development and launch verification such as sine, random and acoustic vibration testing and lessons learned.

Date

2014-09-29

Time

15:15

Room

713A

IPC members
papers

Order

Time

Paper title

Selection result

Mode

Presentation status

Speaker

Affiliation

Country

1

The THOR Space Station at EML2: analysis and preliminary design an innovative adaptable docking system.

accepted

12'

confirmed

Prof. Stéphanie Lizy-Destrez

SUPAERO- Ecole Nationale Supérieure de l'Aéronautique et de l'Espace

France

2

verification and validation for the thermo-mechanical design of ultra high temperature ceramic (uhtc) winglets of a re-entry space vehicle

accepted

12'

confirmed

Dr. ROBERTO SCIGLIANO

CIRA Italian Aerospace Research Centre

Italy

4

Space qualification test of vibration isolator for low amplitude vibration

accepted

12'

confirmed

Mr. Geeyong Park

Korea Advanced Institute of Science and Technology (KAIST)

Korea, Republic of

5

METHOD OF WEIGHT OPTIMIZATION OF DISCRETELY LOADED ROCKET BAYS OF WAFFLE STRUCTURE

accepted

12'

no-show

Mr. Vitaliy Danchenko

Yuzhnoye State Design Office

Ukraine

6

Acoustic performance of foam filled honeycomb sandwich structures

accepted

12'

withdrawn

Dr. R. Ramesh Kumar

Indian Space Research Organization (ISRO)

India

7

development of a metal corrugated diaphragm tank for use in liquid bipropellant propulsion systems

accepted

12'

no-show

Dr. Fei Yan

Shanghai Institute of Space Propulsion

China

8

Equivalent Stiffness Approach (ESAF) for Two Dimensional Analysis of Flanged Joints of Solid Rocket Motors

accepted

12'

no-show

Mr. Sri S. Somanath

Vikram Sarabhai Space Centre (VSSC)

India

9

analysis method of structural fracture behavior

accepted

12'

no-show

Mr. Xibo Wang

Beijing Institute of Aerospace Systems Engineering, China Aerospace Science and Technology Corporation (CASC)

China

10

robust tracking control of dual-arm flexible joint space robot based on backstepping technology

accepted

12'

no-show

Dr. Jie Liang

China

12

performance investigation of solid and solid-grease hybrid lubricated harmonic drive gears under thermal-vacuum environment

accepted

12'

confirmed

12

The Satellite Topology Optimization of Truss Structure and Its Size Sensitivity Analysis

accepted

12'

confirmed

Mr. Huang Fan

Shanghai Institute of Satellite Engineering

China

13

Lateral-staging space launch vehicles dynamics with allowance for propellant crossfeed

accepted

12'

withdrawn

Mr. Arseniy Pavlov

Bauman Moscow State Technical University

Russian Federation