PEASSS thermal subsystem: challenges in the thermal design of CubeSat missions
Date
2015-07-12
Authors
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Publisher
45th International Conference on Environmental Systems
Abstract
PEASSS is a 3-unit CubeSat (slated for launch in 2016) aiming to qualify and test in space “smart structures” including composite panels and piezoelectric materials, new piezo power generation system and fiber-optic sensor plus interrogator system, resulting in a considerable amount of new technology demonstration components. The broader goal of the thermal subsystem responsible is to develop a cost- and resource-efficient approach for the thermal design which can be applied also to small-budget missions like CubeSats and to reduce the risks of the mission related to the extensive use of COTS and not-qualified materials and components typical in CubeSats’ missions.
Description
Bellevue, Washington
The 45th International Conference on Environmental Systems was held in Bellevue, Washington, USA on 12 July 2015 through 16 July 2015.
L. Celotti, Active Space Technologies GmbH, Germany
M. Sołyga, Active Space Technologies GmbH, Germany
B. Cefalo, Active Space Technologies GmbH, Germany
The 45th International Conference on Environmental Systems was held in Bellevue, Washington, USA on 12 July 2015 through 16 July 2015.
L. Celotti, Active Space Technologies GmbH, Germany
M. Sołyga, Active Space Technologies GmbH, Germany
B. Cefalo, Active Space Technologies GmbH, Germany