session 1

Title: Space Structures I - Development and Verification (Space Vehicles and Components)
type: oral
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

Co-Chair: Mr. Alwin Eisenmann, IABG Industrieanlagen - Betriebsgesellschaft mbH, Germany;
Co-Chair: Dr. Andreas Rittweger, DLR (German Aerospace Center), Germany;
Rapporteur: Dr. Jochen Albus, ArianeGroup, Germany;

papers
Order	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	The THOR Space Station at EML2: analysis and preliminary design an innovative adaptable docking system.	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	12'	confirmed	Dr. ROBERTO SCIGLIANO	CIRA Italian Aerospace Research Centre	Italy
4	Space qualification test of vibration isolator for low amplitude vibration	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	12'	no-show	Mr. Vitaliy Danchenko	Yuzhnoye State Design Office	Ukraine
6	Acoustic performance of foam filled honeycomb sandwich structures	12'	withdrawn	Dr.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	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	12'	no-show	Mr. Sri S. Somanath	Vikram Sarabhai Space Centre (VSSC)	India
9	analysis method of structural fracture behavior	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	12'	no-show	Dr. Jie Liang		China
12	performance investigation of solid and solid-grease hybrid lubricated harmonic drive gears under thermal-vacuum environment	12'	confirmed	Prof. hui zhou	China Academy of Space Technology (CAST)	China
12	The Satellite Topology Optimization of Truss Structure and Its Size Sensitivity Analysis	12'	confirmed	Mr. Huang Fan	Shanghai Institute of Satellite Engineering	China
13	Lateral-staging space launch vehicles dynamics with allowance for propellant crossfeed	12'	withdrawn	Mr. Arseniy Pavlov	Bauman Moscow State Technical University	Russian Federation

session 1

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