session 1
- Title
Space Structures I Design, Development and Verification (Launch Vehicles and Space Vehicles, including their Mechanical/Thermal/ Fluidic Systems)
- type
oral
- Description
The topics addressed in this session cover the aspects of the design, development and verification of space launch system structures (e.g. pressurized propellant tanks, non-pressurized structures of space vehicles, control surfaces) and their components (e.g. fluidic equipment and propulsive lines, thermal control systems). The aspects of design, 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) • design, verification and qualification of fluidic and thermal control systems • 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
2025-09-29
- Time
- Room
- IPC members
Co-Chair: Mr. Alwin Eisenmann, IABG Industrieanlagen - Betriebsgesellschaft mbH, Germany;
Co-Chair: Dr. Jochen Albus, ArianeGroup, Germany;
Rapporteur: Dr. Zijun Hu, China Academy of Launch Vehicle Technology (CALT), China;
Rapporteur: Ms. Coraline Dalibot, Rutherford Appleton Laboratory, United Kingdom;
Order | Time | Paper title | Mode | Presentation status | Speaker | Affiliation | Country |
---|---|---|---|---|---|---|---|
1 | 15:30 | 10 | Mr. Said Mouhaiche | The University of Sydney | Australia | ||
2 | 15:40 | Internally Fastened Manhole Cover for Lightweight Composite Propellant Tanks | 10 | Dr. Youngha Yoon | Korea Aerospace Research Institute (KARI) | Korea, Republic of | |
3 | 15:50 | Study of Axial Compression Bearing Capacity of Stainless Steel Tanks in Reusable Launch Vehicle | 10 | Mrs. Pei Li | LandSpace Technology Corporation Ltd. | China | |
4 | 16:00 | study on a novel spacecraft thermal control system based on phase change heat storage | 10 | Dr. Dong La | Shanghai Institute of Satellite Engineering | China | |
5 | 16:10 | Thermal and Structural Analysis of Space-Based Solar Power Satellites (SBSP) in Geostationary Orbit | 10 | Mr. Fawzan Mohamed Kareem Navaz | Amity University, Dubai | United Arab Emirates | |
6 | 16:20 | 10 | Ms. Danielle McDowell | University of Alabama in Huntsville | United States | ||
7 | 16:30 | 10 | Mr. DINENDRA ARCOT VISWANATH | Politecnico di Milano | Italy | ||
8 | 16:40 | Development of a Thermal Vacuum Optical System for Testing Earth Observation Imagers | 10 | Mr. Nicolaas Vlok van Jaarsveld | Simera Sense | South Africa | |
9 | 16:50 | Composite Materials and Manufacturing Methods for Hydrogen Storage for Space Systems | 10 | Ms. zuleyha savci | Ankara Yıldırım Beyazıt University | Türkiye | |
10 | 17:00 | Multifuctional Energy Dense Structural Composites for Advanced Satellite Systems | 10 | Mr. Shryas Bhurat | U.C. Berkeley | United States | |
11 | 17:10 | 10 | Ms. Farha Hassan Priti | BRAC University | Bangladesh | ||
12 | 17:20 | 10 | Prof. Seyed Mohammad Navid Ghoreishi | Satellite Research Institute, Iranian Space Research Center | Iran | ||
13* | 17:30 | 10 | Mr. Farbod Akhavan Niaki | Planet | United States | ||
14* | 17:30 | Damage Identification Model of Re-entry Capsule Based on Field Information Inversion | 10 | Mr. Jia-Xin Hu | Northwestern Polytechnical University | China |