Abstract
Tribolab is a materials tribology experiment that was flown on the International Space
Station (ISS) from February 2008 to September 2009. The main objective of the experiment was the
study of the behaviour of new solid lubricants (alloyed MoS2 with WC) under real space conditions.
The thermal control of the instrument (techniques needed to ensure that the temperature range of the experiment components are adequate in all the mission possible scenarios) was designed, assembled, integrated and tested by a team of engineers of Inasmet-Tecnalia and INTA. The design concept employed, mainly passive thermal control with some active components, is explained in detail. The computational models devised for the design, as well as the different mission scenarios are also explained. The verification and on earth qualification tests are described and the difficulties encountered during the project for the thermal subsystem are also explained. Finally, the real thermal behaviour of the experiment when on space is described, with some post-flight information.
Original language | English |
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Publication status | Published - May 2012 |
Keywords
- Space Thermal Control
- International Space Station
- ISS
- Computational simulation
Project and Funding Information
- Funding Info
- Ministry of Science and Technology, National Plan for Space reference ESP2003-07234._x000D_Ministry of Education and Culture, National Plan for Space reference ESP2007-65130.