session 1
Space Structures I - Development and Verification (Space Vehicles and Components)
- type
oral
- Description
The topics addressed in this session cover the aspects of the development and verification of space vehicle structures (e.g. pressurized propellant tanks, non-pressurized structures of space vehicles, control surfaces) and their components (e.g. fluidic equipment and propulsive lines). The aspects of development, verification and qualification concern: • Thermo-Mechanical loads and environment • New structural concepts (e.g. multi-functional structures, design concepts for reusability) • Structure design and verification (stiffness, strength, static and dynamic stability, damage tolerance, reusability) • Structure optimization • Materials • Static and dynamic ground testing • Exploitation of flight measurements and in-orbit testing • Lessons learned related to space vehicle structures and components development, verification and qualification
- Date
2021-10-25
- Time
- Room
- 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;
Order | Time | Paper title | Mode | Presentation status | Speaker | Affiliation | Country |
---|---|---|---|---|---|---|---|
1 | 15:15 | Thermal Vacuum and Balance Test Method and Validation on Optical Payload | 10 | confirmed | Mr. Mohamed Alsalami | Mohammed Bin Rashid Space Centre (MBRSC) | United Arab Emirates |
4 | 15:25 | 10 | confirmed | Mr. Jeffrey Valania | Sierra Space | United States | |
7 | 15:35 | A global-local approach for the free-edge analysis of composite structures under thermal loads | 10 | confirmed | Dr. Enrico Zappino | Politecnico di Torino | Italy |
8 | 15:45 | Thermal insulation foam for the high precision thermal modeling of space satellites | 10 | confirmed | Mr. Nikolay Mullin | Skolkovo Institute of Science and Technology | Russian Federation |
11 | 15:55 | 10 | withdrawn | Dr. Nikolay Asmolovskiy | Space Structures GmbH | Germany | |
12 | 16:05 | Design and Qualification of a Lightweight Payload Module Optimized for Payload and AIT Flexibility | 10 | confirmed | Mr. Thomas A. Schervan | RWTH Aachen University | Germany |
1002 | 16:15 | 10 | confirmed | Dr. Bhaskar Mukherjee | The University of Sydney | Australia | |
1003 | 16:25 | structure modelling and optimal configuration of a microsatellite in equatorial orbit | 10 | confirmed | Mr. Poki Agung Budiantoro | Indonesian National Institute of Aeronautics and Space (LAPAN) | Indonesia |
1005 | 16:35 | The development of a cryogenic propellant tank fully made of composite materials | 10 | confirmed | Mr. Pavlo Galagan | Yuzhnoye State Design Office | Ukraine |
1006 | 16:45 | Cross-longitudinal reinforcement design for thin structures in aerospace inspired by dragonfly wing | 10 | confirmed | Mr. Hiroki Kawabe | The University of TOKYO, Graduate school | Japan |
1009 | 16:55 | evaluation of shape and solar radiation torque of boom extendable membrane structure with devices | 10 | confirmed | Ms. Ayaka Fujita | Tokai University | Japan |
1010 | 17:05 | 10 | withdrawn | Mr. Nikolay Mullin | Skolkovo Institute of Science and Technology | Russian Federation | |
* | Aerothermal analysis and thermal protection of grid fins for reentry rockets | Dr. Liang CHEN | Beijing Interstellar Glory Space Technology Co., Ltd | China |