Spacecraft Radiator Freeze Protection Using a Regenerative Heat Exchanger

TBMG-9447

03/09/2011

Abstract
Content

An active thermal control system architecture has been modified to include a regenerative heat exchanger (regenerator) inboard of the radiator. Rather than using a radiator bypass valve, as illustrated in (a), a regenerative heat exchanger is placed inboard of the radiators as shown in (b). A regenerator cold side bypass valve is used to set the return temperature.

Meta TagsDetails
Citation
"Spacecraft Radiator Freeze Protection Using a Regenerative Heat Exchanger," Mobility Engineering, March 9, 2011.
Additional Details
Publisher
Published
Mar 9, 2011
Product Code
TBMG-9447
Content Type
Magazine Article
Language
English