Abstract:
Constructive-functional elaboration of the strength structure of the TUMnanoSAT microsatellite. Elaboration of the calculation model and computerized simulation of the load factors according to the operating criteria in the real space conditions; Development and manufacture of microsatellite assembly transport and vibration testing devices according to the technical and technological requirements of the Japan Space Exploration Agency (JAXA).
Description:
Istitution: Technical University of Moldova. Project Nr. 20.80009.5007.09 "Development and launch of the series of nanosatellites with research missions on the International Space Station, monitoring, postoperating and promoting space technologies".