Browse Publications Technical Papers 2000-01-2411
2000-07-10

Modeling and Test Results for Two Loop Heat Pipes with a Freeze-Tolerant Condenser 2000-01-2411

This paper describes modeling and test results for a two Loop Heat Pipes (LHP) with a condenser designed to be used in a deployable spacecraft radiator system. These units were provided by the two major commercial US vendors of LHPs. The condenser used is a freeze-tolerant, parallel-flow design based on the International Space Station (ISS) deployable radiator design. This condenser allows the deployable radiator to be utilized without freeze-protection heaters.

SAE MOBILUS

Subscribers can view annotate, and download all of SAE's content. Learn More »

Access SAE MOBILUS »

Members save up to 18% off list price.
Login to see discount.
Special Offer: Download multiple Technical Papers each year? TechSelect is a cost-effective subscription option to select and download 12-100 full-text Technical Papers per year. Find more information here.
We also recommend:
TECHNICAL PAPER

Modeling and Design of Optimal Growth Media from Plant - Based Gas and Liquid Fluxes

2005-01-2949

View Details

TECHNICAL PAPER

International Space Station Alpha Design-To-Freeze Radiators

951652

View Details

TECHNICAL PAPER

Numerical and Experimental Study of Three Dimensional Flow in Engine Room

960270

View Details

X