Thermal Performance of Embedded Heat Pipe Spacecraft Radiator Panels

932158

07/01/1993

Event
International Conference On Environmental Systems
Authors Abstract
Content
The embedded heat pipe radiator panel is the thermal foundation for the present and future-generation three-axis-stabilized, geosynchronous communications spacecraft. This paper discusses design guidelines and analyzes the thermal performance of some commonly used heat pipe/panel configurations. Among the designs considered are an in-plane design with heat pipes bonded to each other in overlapping sections, an in-plane design with heat pipes crossing on two levels, and externally mounted heat pipes. The thermal performance parameters are quantified and compared as a function of radiator area and weight.
Meta TagsDetails
DOI
https://doi.org/10.4271/932158
Pages
8
Citation
Kelly, W., and Reisenweber, J., "Thermal Performance of Embedded Heat Pipe Spacecraft Radiator Panels," SAE Technical Paper 932158, 1993, https://doi.org/10.4271/932158.
Additional Details
Publisher
Published
Jul 1, 1993
Product Code
932158
Content Type
Technical Paper
Language
English