TY - GEN
T1 - Phase-Change Material Thermal Management for Extreme Space Environments
AU - Bennett, Nick S.
AU - Raffa, Laryssa Sueza
AU - Arqam, Mohammad
AU - Ould, Solomon
AU - Clemon, Lee
N1 - Publisher Copyright:
Copyright © 2025 by the International Astronautical Federation (IAF). All rights reserved.
PY - 2025
Y1 - 2025
N2 - Thermal management is essential for the extreme environments of space - vital in order to conduct successful missions, make new discoveries, and push the boundaries of space exploration. Without adequate temperature control systems, astronauts and equipment can be exposed to extreme temperatures that could cause equipment failure, decreased performance, and even risk human life. Thermal control systems come in a range of varieties but include those based on phase-change materials (PCMs), which are passive, reliable and effective, if properly designed. PCMs are particularly attractive due to their unique ability to protect against both hot and cold temperature extremes by absorbing, storing, and releasing thermal energy during temperature cycling, thus maintaining a stable thermal environment. In space, it is essential that the PCM is housed within a suitably robust container - preferably one that allows rapid heat transfer from the heat source to the PCM. Here, we report on key learnings from our team's additive-manufactured (AM) PCM-heat sink, namely the “Matilda” payload, launched to low-Earth orbit on Waratah Seed-1. Specifically, we report on the necessary compromises encountered between the heat transfer benefits resulting from complex thermal conductivity-enhancing structures enabled by AM, and the additional manufacturing challenges resulting from AM.
AB - Thermal management is essential for the extreme environments of space - vital in order to conduct successful missions, make new discoveries, and push the boundaries of space exploration. Without adequate temperature control systems, astronauts and equipment can be exposed to extreme temperatures that could cause equipment failure, decreased performance, and even risk human life. Thermal control systems come in a range of varieties but include those based on phase-change materials (PCMs), which are passive, reliable and effective, if properly designed. PCMs are particularly attractive due to their unique ability to protect against both hot and cold temperature extremes by absorbing, storing, and releasing thermal energy during temperature cycling, thus maintaining a stable thermal environment. In space, it is essential that the PCM is housed within a suitably robust container - preferably one that allows rapid heat transfer from the heat source to the PCM. Here, we report on key learnings from our team's additive-manufactured (AM) PCM-heat sink, namely the “Matilda” payload, launched to low-Earth orbit on Waratah Seed-1. Specifically, we report on the necessary compromises encountered between the heat transfer benefits resulting from complex thermal conductivity-enhancing structures enabled by AM, and the additional manufacturing challenges resulting from AM.
KW - Additive manufacturing
KW - CubeSat
KW - Phase-change material
KW - Thermal management
UR - https://www.scopus.com/pages/publications/105035991080
U2 - 10.52202/083088-0039
DO - 10.52202/083088-0039
M3 - Conference contribution
AN - SCOPUS:105035991080
T3 - Proceedings of the International Astronautical Congress, IAC
SP - 360
EP - 367
BT - IAF Materials and Structures Symposium - Held at the 76th International Astronautical Congress, IAC 2025
PB - International Astronautical Federation, IAF
T2 - 2025 IAF Materials and Structures Symposium at the 76th International Astronautical Congress, IAC 2025
Y2 - 29 September 2025 through 3 October 2025
ER -