session 7
- Title
Space Vehicles – Mechanical/Thermal/Fluidic Systems
- type
oral
- Description
The topics to be addressed include novel technical concepts for mechanical/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.
- Date
2016-09-29
- 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;
Order | Time | Paper title | Mode | Presentation status | Speaker | Affiliation | Country |
|---|---|---|---|---|---|---|---|
1 | Future Actuator development - a new approach and first results | 15' | confirmed | Dr. Oliver Kunz | RUAG Space AG | Switzerland | |
3 | the thermal analysis of lapan’s ir micro bolometer optical design | 15' | confirmed | Mr. Bustanul Arifin | Indonesian Space Agency Secretariat (INASA) | Indonesia | |
7 | 15' | confirmed | Mr. Marco Vietze | Universität der Bundeswehr München | Germany | ||
9 | Thermal-Vacuum Tests of the Amazonia-1 Satellite TM Performed at INPE With Success | 15' | confirmed | Dr. Jose Sergio Almeida | The Brazilian Institute for Space Research - INPE | Brazil | |
10 | 15' | confirmed | Prof. Bingyan Chen | China Academy of Aerospace Aerodynamics (CAAA) | China |
