Principles of Thermostable Heat Pipe 3-D Girder Design

972454

07/01/1997

Event
International Conference On Environmental Systems
Authors Abstract
Content
It's considered an approach to the elaboration of the tubing truss construction for payload accomodation on spacecraft which except support functions can fulfill the heat pipe function - to redistribute heat flows quickly and to equalize temperatures between heated and cold parts of the girder. The eventual thermal state of such constructions is analyzed in circumstances of space operation and in the course of on-Earth tests.
Results of compatibility tests of casing material (aluminum alloy AMg-6) and heat-transfer agent (ammonia) at prolonged exploitation are presented.
Meta TagsDetails
DOI
https://doi.org/10.4271/972454
Pages
7
Citation
Dranovskiy, V., Gladilin, V., Tarasov, G., Tikhiy, V. et al., "Principles of Thermostable Heat Pipe 3-D Girder Design," SAE Technical Paper 972454, 1997, https://doi.org/10.4271/972454.
Additional Details
Publisher
Published
Jul 1, 1997
Product Code
972454
Content Type
Technical Paper
Language
English