Practical Considerations of Integrating a Passive Thermal Control System onto Small-Satellites - The Ten-Koh Case Study

Date

2020-07-31

Authors

Dudziak, Roger
Tuttle, Sean
Okuyama, Kei-Ichi
Lidtke, Aleksander
Gonzales, Jesus
Fajardo Tapia, Isai

Journal Title

Journal ISSN

Volume Title

Publisher

2020 International Conference on Environmental Systems

Abstract

The research detailed in this paper aims to address the problem of thermal management of small-satellite (particularly micro and nano-satellite) platforms by proposing a passive Thermal Management System (TMS) that can be integrated onto existing satellite designs. This characteristic will be highlighted through discussion of the work undertaken to integrate elements of the TMS onto the recently launched Ten-Koh micro-satellite. This integration was conducted to allow an on-orbit demonstration of the passive switch component where a highly dissipating payload is used as the heat source.

The TMS is comprised of three key components. These include a heat strap manufactured from Pyrolitic Graphite Sheet (PGS), a thermal switch activated by Shape Memory Alloy (SMA) and a multi-layered PGS radiator, folded to provide maximum radiative surface area once deployed from an external face of the small-satellite.

Breadboard testing of the PGS strap and SMA switch has been conducted, the results of which were presented at ICES 2017 . This testing characterised heat transfer through the PGS as a function of strap thickness and interface pressure. It also showed that, while the prototype SMA switch generated sufficient interface pressure to allow good heat transfer through the strap, further development was required to improve reliability. Since ICES 2017, significant development of the switch has been undertaken to allow successful integration onto the Engineering and Flight Models of the Ten-Koh recently launched by JAXA. Specifically, an intensive development period was undertaken to ensure that the switch was sufficiently robust to pass all of the JAXA safety and qualification tests prior to launch. This included shock, vibration and system-safety testing. Additional integration work was also carried out to ensure that the pressure and temperature sensors which will provide telemetry data on-orbit, successfully integrated with the satellite's on board computer.

Description

Roger Dudziak, Nano Thermal Technologies, AU
Sean Tuttle, Nano Thermal Technologies, AU
Kei-Ichi Okuyama, Nihon University, JP
Aleksander Lidtke, Kyushu Institute of Technology, JP
Jesus Gonzales, Kyushu Institute of Technology, JP
Isai Fajardo Tapia, Kyushu Institute of Technology, JP
ICES107: Thermal Design of Microsatellites, Nanosatellites, and Picosatellites
The proceedings for the 2020 International Conference on Environmental Systems were published from July 31 – August 6, 2020. The technical papers were not presented in person due to the inability to hold the event as scheduled in Lisbon, Portugal because of the COVID-19 global pandemic.

Keywords

Passive, Thermal, Control

Citation