session 7
Space Vehicles – Mechanical/Robotic/Thermal/Fluidic Systems
- type
oral
- Description
The topics to be addressed include novel technical concepts for mechanical/robotic/thermal/fluidic systems and subsystems of launchers, manned and unmanned spacecraft, re-entry vehicles and small satellites. Advanced subsystems and design of future exploration missions will be covered, considering issues arising from material selection, cost efficiency and reliability, and advancements in space vehicle development with respect to engineering analysis, manufacturing, and test verification. It is also planned to discuss the issues of experimental and computational simulation of functioning and full-scale tests of space vehicles and their systems/subsystems. Attention will be paid to the problem of verification and validation of mathematical models for the design and experimental development of these objects at various phases of their life cycle.
- Date
2022-09-21
- Time
- Room
- IPC members
Co-Chair: Dr. Brij Agrawal, Naval Postgraduate School, United States;
Co-Chair: Prof.Dr. Oleg Alifanov, MAI, Russian Federation;
Rapporteur: Prof. Guoliang Mao, Beijing Institute of Aerodynamics, China;
Rapporteur: Dr. Federica Angeletti, University of Rome “La Sapienza”, Italy;
Order | Time | Paper title | Mode | Presentation status | Speaker | Affiliation | Country |
---|---|---|---|---|---|---|---|
1 | 15:00 | 12 | confirmed | Mr. Maxime HEGO | France | ||
2 | 15:12 | Experimental Validation of a Solid State Magnetocaloric Cooler in a Space Environment | 12 | confirmed | Mr. Markus Huwald | Technische Universität Braunschweig, Institute of Space Systems | Germany |
3 | 15:24 | Analysis of effective thermal control designs for small satellites | 12 | confirmed | Ms. Anvesha Yadav | R.V.College of Engineering | India |
4 | 15:36 | 12 | confirmed | Dr. wenbin cao | LandSpace Technology Corporation Ltd. | China | |
5 | 15:48 | thermal balance and thermal vacuum test of the cbers-4a satellite performed at inpe, brazil. | 12 | confirmed | Dr. Geilson Loureiro | National Institute for Space Research - INPE | Brazil |
6 | 16:00 | 12 | confirmed | Ms. Spoorthi M.S. | University of Petroleum and Energy Studies | India | |
7 | 16:12 | Temperature distribution along a composite and metallic shell in cryogenic environment | 12 | confirmed | Mr. Prashumn Prashumn | Indian Space Research Organization (ISRO), Liquid Propulsion Systems Centre (LPSC) | India |
8 | 16:24 | Influence of hydrogen and oxygen self-pressurizing temperature on heat transfer of propellant tank | 12 | confirmed | Dr. Liqiang Ai | China Academy of Launch Vehicle Technology (CALT) | China |
9 | 16:36 | 12 | confirmed | Ms. Juliette Lacasse | Université de Sherbrooke | Canada | |
10 | 16:48 | Structural design of a CubeSat type nanosatellite for academic purposes. | 12 | confirmed | Mr. Edwin Cruz Martínez | Mexico | |
11 | 17:00 | 12 | confirmed | Ms. Jana Catuche | United States | ||
12 | 17:12 | The fabrication and application of water sublimator heat dissipation system in Chang'e 5 lunar probe | 12 | Dr. Yuying WANG | Beijing Institute of Spacecraft System Engineering, China Academy of Space Technology | China |