Design Summary of the Insat Lightweight, Deployable Solar Array

821397

02/01/1982

Event
Aerospace Congress and Exposition
Authors Abstract
Content
The Insat-1 satellite will provide a significant development in solar ray technology for synchronous orbit high power satellites. It is a three-axis stabilized spacecraft designed for seven year operation to provide communications/meteorological service to India. Primary energy source is a single-axis, single-tracking solar array wing with solar torque offset by an opposing solar sail boom. The solar array, composed of five graphite epoxy rigid deployable panels, provides 1000 W divided between two separate power buses.
Meta TagsDetails
DOI
https://doi.org/10.4271/821397
Pages
11
Citation
Barberis, N., Dixson, J., and Woytowitz, P., "Design Summary of the Insat Lightweight, Deployable Solar Array," SAE Technical Paper 821397, 1982, https://doi.org/10.4271/821397.
Additional Details
Publisher
Published
Feb 1, 1982
Product Code
821397
Content Type
Technical Paper
Language
English