Aerospace
Technical Paper

Development Status of a Two-Phase Thermal Management System for Large Spacecraft

861828

10/01/1986

Event
SAE Aerospace Technology Conference and Exposition
Authors
Timothy J. Bland Sundstrand Corp., Rockford, IL
Ing-Yomn Chen Sundstrand Corp., Rockford, IL
David G. C. Hill Sundstrand Corp., Rockford, IL
Abstract
Content
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.
Meta Tags
Topics
Thermal management
Hardware
Microgravity
Simulation and modeling
Affiliated or Co-Author
Sundstrand Corp., Rockford, IL
Details
DOI
https://doi.org/10.4271/861828
Pages
12
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.
Additional Details
Publisher
SAE International
Published
Oct 1, 1986
Product Code
861828
Content Type
Technical Paper
Language
English