One Year Operations of the MITA Mini-Satellite–Validation of the Thermal Design from On-Orbit Data

An experimental campaign is presented aiming at the characterization of thermal dissipation of batteries to be used on board of small satellites. A suitably designed device allows to manage automatically the orbital cycling simulation between battery cell charge and discharge. The cell thermal performance is characterized in various combinations of temperature, discharge current and Depth of Discharge. The gathered data are used for providing guidelines in the design of a family of Italian Small Satellites

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In-Flight Results of the Sciamachy Optical Assembly Active Thermal Control System

Lemmen¹,

Kouwen²,

Koorevaar³

et al. 2004

SAE Technical Paper Series

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One Year Operations of the MITA Mini-Satellite–Validation of the Thermal Design from On-Orbit Data

Cited by 4 publications

References 1 publication

Satellite Thermal Engineering - lessons from ICES

Satellite Thermal Engineering - lessons from ICES

Experimental Characterization of Power Dissipation of Battery Cells for Space Environment

In-Flight Results of the Sciamachy Optical Assembly Active Thermal Control System

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