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Solid-State Distributed Temperature Control for International Space Station
Technical Paper
2004-01-2430
ISSN: 0148-7191, e-ISSN: 2688-3627
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English
Abstract
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.
Authors
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.Also In
References
- The International Space Station’s Multi-Purpose Logistics Module: Thermal Performance of the First Five Flights
- An Integrated Approach to Thermal Management of International Space Station Logistics Flights: Improving the Efficiency
- Programmable Thermostat End Item Specification
- Data Recorder End Item Specification
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- Heaters and Thermostats (TCS S/S) Stress Analysis 09 Sep 1997
- MPLM Baseline Configuration Report 31 March 1998
- SINDA/Fluint General Purpose Thermal/Fluid Netwrok Analyzer July 2001