Hybrid Honeycomb Panel Heat Rejection System

871419

07/01/1987

Event
Intersociety Conference on Environmental Systems
Authors Abstract
Content
The evolution of a hybrid honeycomb panel heat rejection system concept for future high-power spacecraft is described. Performance evaluation of this heat pipe-based hybrid radiator is based on data and prediction models from a developmental component hardware testing program. The concept integrates three high-performance components into an optimized radiator system. These components are the sideflow heat pipe transport leg, honeycomb panel evaporator, and light-weight high-efficiency heat pipe fins. A 3.05 m (10 ft.) long hybrid radiator was designed considering remnant hardware available from other Hughes programs. Key performance objectives for the hybrid radiator were to demonstrate high thermal transport capacity, increased radiating fin lengths, improved thermal efficiency across structural boundaries, and reduced weight. Analysis showed that 9000 W can be transported over a 3.05 m radiator and that fin lengths of up to 1 m are possible.
Meta TagsDetails
DOI
https://doi.org/10.4271/871419
Pages
15
Citation
Tanzer, H., and Hall, J., "Hybrid Honeycomb Panel Heat Rejection System," SAE Technical Paper 871419, 1987, https://doi.org/10.4271/871419.
Additional Details
Publisher
Published
Jul 1, 1987
Product Code
871419
Content Type
Technical Paper
Language
English