Development of Two-Phase Fluid Loop Systems for Future Space Platforms

891470

07/01/1989

Event
Intersociety Conference on Environmental Systems
Authors Abstract
Content
Since 1985 NASDA has made studies on advanced thermal management systems, especially on two-phase fluid loops, with a view to applying to temperature control and heat rejection of future space platforms of tens of kW class. Our research on pump-driven two-phase fluid loop technology is in a new stage where we have completed the design and fabrication of a development model. This paper describes the loop system design and gives details of components, which are three kinds of cold plates (grooved double-pipe type, grooved multi-channel type, tube and plate-heat-pipe type), two kinds of volumetric pumps (trochoid gear type, scroll type) and an accumulator of vapor pressure driven type. This paper, then, gives a brief description of an X-ray void meter which we have prepared for measurements of void fractions and for graphical observations of various flow patterns in the cold plates.
Meta TagsDetails
DOI
https://doi.org/10.4271/891470
Pages
11
Citation
Ishii, Y., Furukawa, M., Miyazaki, Y., Kuriyama, Y. et al., "Development of Two-Phase Fluid Loop Systems for Future Space Platforms," SAE Technical Paper 891470, 1989, https://doi.org/10.4271/891470.
Additional Details
Publisher
Published
Jul 1, 1989
Product Code
891470
Content Type
Technical Paper
Language
English