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
2019-10-21
- 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 | 15:00 | Development & Testing of the Single-Person Spacecraft Crew Enclosure | 12 | confirmed | Mr. Matthew Stephens | National Aeronautics and Space Administration (NASA), Goddard Space Flight Center | United States |
2 | 15:12 | 12 | withdrawn | Ms. Erika Lieberknecht | United States | ||
3 | 15:24 | Fracture Control for Additively Manufactured Spacecraft Structures | 12 | confirmed | Dr. Mark McElroy | National Aeronautics and Space Administration (NASA) | United States |
4 | 15:36 | modeling of additive manufactured heat pipes for advanced small satellite design | 12 | confirmed | Mr. Nikolay Mullin | Skolkovo Institute of Science and Technology | Russian Federation |
5 | 15:48 | development of H3 launch vehicle 1st stage engine section structure | 12 | confirmed | Mr. Hiroki Hamajima | MHI | Japan |
6 | 16:00 | ARIANE 6 UPPER LIQUID PROPULSION MODULE THERMAL PROTECTION HARDWARE DEVELOPMENT AND TESTING | 12' | confirmed | Mr. Arturs Jasjukevics | ArianeGroup | Germany |
7 | 16:12 | 12 | confirmed | Mr. Khaja Fayaz Hussain | Scuola di Ingegneria Aerospaziale "La Sapienza" | Italy | |
8 | 16:24 | development of large high pressurized xenon tank for electrical propulsion systems | 12 | confirmed | Mr. Aicke Patzelt | MT Aerospace AG | Germany |
9 | 16:36 | A Condensation Approach for Virtual Shaker Testing Procedures | 12 | confirmed | Dr. Marcello Remedia | Surrey Space Centre, University of Surrey | United Kingdom |
10 | 16:48 | Node-Dependent Kinematic Models for the Coupled Load Analysis of Space Structures | 12 | confirmed | Dr. Enrico Zappino | Politecnico di Torino | Italy |
11 | 17:00 | A new device and method for simulating hypersonic aerothermal Environment | 12 | withdrawn | Prof.Dr. Dechuan Sun | School of Aeronautics and Astronautics, Dalian University of Technology | China |
12 | 17:12 | 12 | confirmed | Mr. Siva kumar Ganesan | Indian Space Research Organization (ISRO) | India | |
* | SLS Production Friction Stir Plugs by Solid State Additive Deposition | Ms. Kathryn Anderson | The University of Alabama | United States | |||
* | topology optimization for lightweighting of components considering manufacturing variabilities | Mr. Alberto Torres | The John Hopkins University | United States | |||
* | Use of nondimensional buckling equations for launch vehicle structures design | Ms. Ines Uriol Balbin | Delft University of Technology (TU Delft) | The Netherlands |