Solid-State Distributed Temperature Control for International Space Station 2004-01-2430
A newly developed solid-state temperature controller will offer greater flexibility in the thermal control of aerospace vehicle structures. A status of the hardware development along with its implementation on the Multi-Purpose Logistics Module will be provided. Numerous advantages of the device will also be discussed with regards to current and future flight vehicle implementations.
Citation: Holladay, J., Reagan, S., and Day, G., "Solid-State Distributed Temperature Control for International Space Station," SAE Technical Paper 2004-01-2430, 2004, https://doi.org/10.4271/2004-01-2430. Download Citation
Author(s):
Jon B. Holladay, Shawn E. Reagan, Greg Day
Affiliated:
NASA/Marshall Space Flight Center
Pages: 7
Event:
International Conference On Environmental Systems
ISSN:
0148-7191
e-ISSN:
2688-3627
Related Topics:
Hardware
Logistics
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