Development Status of a Two-Phase Thermal Management System for Large Spacecraft 861828
An update of a Two-Phase Thermal Management System concept is presented including hardware status for flight prototypic components, modeling techniques, and terrestrial test results for both preprototype and some prototypic hardware. A test plan for a microgravity test on a KC 135 is discussed.
Citation: Bland, T., Chen, I., and Hill, D., "Development Status of a Two-Phase Thermal Management System for Large Spacecraft," SAE Technical Paper 861828, 1986, https://doi.org/10.4271/861828. Download Citation
Author(s):
Timothy J. Bland, Ing-Yomn Chen, David G. C. Hill
Affiliated:
Sundstrand Corp., Rockford, IL
Pages: 12
Event:
SAE Aerospace Technology Conference and Exposition
