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Published in:
Introduction to the Microsatellite Platform Read chapter Read first chapter

2016 | OriginalPaper | Chapter

8. Thermal Control Subsystem

Authors : Fabian Steinmetz, Sebastian Keil

Published in: The FLP Microsatellite Platform

Publisher: Springer International Publishing

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Abstract

The chapter provides an overview on the platform thermal control subsystem. It explains the placement of thermal equipment over the diverse satellite compartments at hand of an example FLP-based spacecraft. It explains the logic of component operational and non operational limits, the allocated sensors, sensor redundancies, allocated compartment heaters and heater redundancies. The last part comprises the onboard software elements and functions for control of the thermal subsystem.

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previous chapter Attitude Control Subsystem
next chapter Payload Control Subsystem
Footnotes
1
The battery compartment is treated as a dedicated own “Module” by the thermal control algorithm, as the battery is thermally decoupled from the spacecraft. More details are provided in Sect. 8.3.2.3.
 
2
To be entirely precise: The actual rule is that for every device handler which controls a device that must be thermally monitored, there is a thermal component. The only exception is the OBC which only has one thermal component for each redundant OBC side although it has more equipment device handlers.
 
Metadata
Title
Thermal Control Subsystem
Authors
Fabian Steinmetz
Sebastian Keil
Copyright Year
2016
Book
The FLP Microsatellite Platform

Print ISBN: 978-3-319-23502-8

Electronic ISBN: 978-3-319-23503-5

Copyright Year: 2016

DOI
https://doi.org/10.1007/978-3-319-23503-5_8

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