session 1
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
2024-10-14
- 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 | confirmed | Ms. Bianca Omede' | Politecnico di Milano | Italy | |
2 | 15:40 | Nozzle Extension Concept Design of AVIO’s Liquid Rocket Engine | 10 | withdrawn | Mr. Nicolò Maria Frisone | AVIO S.p.A. | Italy |
3 | 15:50 | Prediction of Thermo-Mechanical State of Reentry Capsule Based on Limited Sensors | 10 | confirmed | Dr. Jian-Jun Gou | Northwestern Polytechnical University | China |
4 | 16:00 | 10 | confirmed | Mr. Marco Ancillai | AVIO S.p.A. | Italy | |
5 | 16:10 | Structural Optimization of a Stiffened Cylinder using Artificial Neural Networks | 10 | confirmed | Mr. S M SHEHZEB ABBAS | Pakistan Space and Upper Atmosphere Research Commission (SUPARCO) | Pakistan |
6 | 16:20 | Numerical study of vibration fatigue failure for pipeline welded structure in liquid rocket engines | 10 | confirmed | Dr. Hanyang Shi | Xi'an Aerospace Propulsion Institute | China |
7 | 16:30 | Development and testing of a thrust vector control system for a hybrid rocket engine | 10 | confirmed | Mr. Patrick Christian Melo | University of Brasilia | Brazil |
8 | 16:40 | 10 | confirmed | Mr. Kuldeep Singh Rajput | Bellatrix Aerospace Private Limited. | India | |
9 | 16:50 | 10 | confirmed | Mr. Wichayuth Klankla | National Astronomical Research Institute of Thailand (NARIT) | Thailand | |
10 | 17:00 | An Evaluation of Composite Primary Structure for Habitat Modules | 10 | confirmed | Mr. bennett torrance | Boeing | United States |
11 | 17:10 | 10 | confirmed | Ms. Yoshino Sakuraba | Tokyo University of Science | Japan | |
12 | 17:20 | 10 | confirmed | Mr. Lorenzo Rabagliati | Italy |