session 1
- Title
 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, Deutsche Gesellschaft für Luft-und Raumfahrt, Lilienthal-Oberth e.V. (DGLR), 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2  | 15:12  | 12  | withdrawn  | Ms.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  | 
