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Current Mechanically Pumped Two-Phase Thermal Control Loop Developments
Technical Paper
2004-01-2507
ISSN: 0148-7191, e-ISSN: 2688-3627
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English
Abstract
After a general introduction on two-phase thermal control system issues, the paper reviews the status of and lists commonalities and differences between the only two currently developed aerospace-related mechanically pumped two-phase thermal control systems. These are the Russian Segment Active Thermal Control System (RSATCS) hybrid two-phase ammonia thermal control system for the Russian segment of the International Space Station ISS, and the Tracker Thermal Control System (TTCS) hybrid two-phase carbon dioxide thermal control loop for the AMS-2 attached ISS payload.
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Citation
Delil, A., "Current Mechanically Pumped Two-Phase Thermal Control Loop Developments," SAE Technical Paper 2004-01-2507, 2004, https://doi.org/10.4271/2004-01-2507.Also In
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