System analysis of deployable components for micro landers in low gravity environment
Programme Reference
15/725
Country
Poland
Start Date
2016
End Date
2017
Programme: Discovery Prime Contractor: Space Research Centre of the Polish Academy of Sciences
Description
The project entitled "System analysis of deployable components for micro landers in low gravity environment" is conducted within the framework of the ESA contract no. 4000117150/16/NL/HK/hh. Its goal is to perform an analysis and trade-off between the various design options for antennas and solar array deployment mechanisms (including a comparison between the fixed and deployable configurations) of the MASCOT-2 lander in the micro-gravity environment of Didymoon. Moreover, a preliminary design of the concept selected based on the Trade-off Report will be performed, and the preparation of the MASCOT-2 deployable components development plan also constitutes a significant part of the project.
• Application domain: Generic Technologies
• Initial TRL: TRL N/A
• Target TRL: TRL N/A
•Public Document:
