Technical programme
IAC-08 — 59th International Astronautical Congress
C2. MATERIALS AND STRUCTURES SYMPOSIUM
This Symposium provides an international forum for recent advancements in assessment of the latest technology achievements on space structures, structural dynamics and materials. The Symposium addresses the design and development of space vehicle structures and mechanical/thermal/fluidic systems. Future advances in a number of space systems applications for space power, space transportation, astrodynamics, space exploration, space propulsion and space station will depend increasingly on the successful application of innovative materials and the development of structural concepts - particularly those relating to very large deployable (and assembled) space structures. For these applications to occur, increased dialog between these technology communities, and discussion among technologists and mission planners, must be pursued. Substantial improvements in a wide range of current technologies, including nanotechnologies, must occur, projected costs must be reduced, potential scientific returns must be increased from respective mission system applications. Papers in this symposium will review the projected advances in materials and large space structures in this domain for advanced space systems applications.
- Coordinator
Constantinos P. Stavrinidis
IABG Industrieanlagen - Betriebsgesellschaft mbH — GermanyPavel M. Trivailo
RMIT University, Australia — Australia
C2.1. Space Structures I - Development and Verification (Space Vehicles and Components)
The following topics will be included: Analysis versus test results for spacecraft, launch vehicles and their components (e.g. pressurized structures, tanks, load introductions, primary structures, fluidic equipment, control surfaces); examination of both on-ground and in-orbit testing, launch dynamic environments as related to structural design, development and verification, such as sine, random and acoustic vibration and lessons learned.
- Chairman
Alwin Eisenmann
IABG Industrieanlagen - Betriebsgesellschaft mbH — GermanyAndreas Rittweger
DLR (German Aerospace Center) — Germany
- Rapporteur
Jean-Alain Massoni
Thales Alenia Space France — France
C2.2. Space Structures II - Development and Verification (Deployable and Dimensionally Stable Structures)
The following topics will be included: Analysis versus test results for deployable and /or 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.
- Chairman
Paolo Gasbarri
University of Rome “La Sapienza” — ItalyJean-Alain Massoni
Thales Alenia Space France — France
- Rapporteur
Pierre Rochus
CSL (Centre Spatial de Liège) — Belgium
C2.3. Space Structures - Dynamics and Microdynamics
Topics included in this session are: Dynamics analysis and testing, modal identification, landing and impact dynamics, pyroshock, test facilities, vibration suppression techniques, damping, micro-dynamics, in-orbit dynamic environment, wave structural propagation, excitation sources and in-orbit dynamic testing.
- Chairman
Peter M. Bainum
Howard University — United StatesIjar Da Fonseca
ITA-DCTA — Brazil
- Rapporteur
Harijono Djojodihardjo
Bandung Institut of Tecnology — Indonesia
C2.4. New Materials and Structural Concepts
Topics of discussion in this session will be: advanced materials and structural concepts applied in expendable and future reusable transportation systems and space vehicles. Of main interests are high temperature and cryogenic materials, nano-materials, composites, and ceramics including their structural application.
- Chairman
Marc Lacoste
ArianeGroup — FranceYuriy Moshnenko
— Ukraine
- Rapporteur
Luigi Scatteia
PricewaterhouseCoopers Advisory (PwC) — France
C2.5. Smart Materials and Adaptive Structures
The focus of the session will be on application of smart materials to spacecraft and launch vehicle systems, novel sensor and actuator concepts and new concepts for multi- functional and intelligent structural systems. Also included in the session will be new control methods for vibration suppression and shape control using adaptive structures as well as comparisons of predicted performance with data from ground and in-orbit testing.
- Chairman
Michael Eiden
ESA (retired) — GermanyJunjiro Onoda
ISAS/JAXA — Japan
- Rapporteur
Paolo Gaudenzi
Sapienza University of Rome — Italy
C2.6. Space Environmental Effects and Spacecraft Protection
In this session space environment effects will be covered. For example, the effects of radiation, atomic oxygen, spacecraft charging, thermal cycling, dissociation, meteoroids, space debris and vacuum on space systems, microelectronics, materials and structures will be discussed. Protective and shielding technologies, including debris impact simulation, testing and susceptibility of Commercial-Off-The-Shelf (COTS) micro-electronics to space radiation will be presented.
- Chairman
Minoo Dastoor
National Aeronautics and Space Administration (NASA) — United StatesAkira Meguro
Tokyo City University — Japan
C2.7. Space Vehicles – Mechanical/Thermal/Fluidic Systems
Discussed in this session are novel technical concepts for mechanical/thermal subsystems of launchers, manned and unmanned spacecraft, re-entry vehicles and small satellites. Also included in this session will be cost efficiency and reliability, material selection, new theoretical approaches, low cost manufacturing and test verification. Advanced subsystems and design for future exploration missions will also be included.
- Chairman
Mario Marchetti
Sapienza University of Rome — ItalyOleg Alifanov
MAI — Russian Federation
- Rapporteur
Guoliang Mao
Beijing Institute of Aerodynamics — China
C2.8. Specialized Technologies, including Nanotechnology
Specialized material and structures technologies are explored in a large variety of space applications both to enable advanced exploration or science/observation mission scenarios and to perform test verifications relying on utmost miniaturization of devices or highest capabilities in structural, thermal, electrical, electro-mechanical/optical performances offered by the progress in Nanotechnology. Examples are the exceptional performances at nano-scale in strength, electrical, thermal conduction of Carbon nanotubes which are experiencing first applications at macro-scale such as nano-composite structures, high efficiency energy storage wheels, MEMS and MOEMS devices. Molecular nanotechnology and advances in manipulation at nano-scale offer the road to molecular machines, ultra-compact sensors for science applications and mass storage devices. The Session encourages presentations of specialized technologies, in particular of nano-material related techniques and their application in devices offering unprecedented performances for space applications.
- Chairman
Mario Marchetti
Sapienza University of Rome — ItalyPierre Rochus
CSL (Centre Spatial de Liège) — Belgium
- Rapporteur
Pavel M. Trivailo
RMIT University, Australia — Australia
C2.I. Interactive Session on Materials and Structures
- Chairman
Michael Eiden
ESA (retired) — Germany