Thermal Design, Testing and On-Orbit Performance of the Italsat Communication Satellites

951749

07/01/1995

Event
International Conference on Environmental Systems
Authors Abstract
Content
The ITALSAT telecommunication system is based on the operation of two geostationary satellites:
  • the first (pre-operative) launched in January '91
  • the second (operative) to be launched in '96.
The thermal design of the satellites was extensively verified by analysis and test including a Solar Simulation thermal balance on the structural-thermal model and thermal vacuum - thermal balance on flight models. Additionally, on-orbit temperature data from the protoflight model is available for equinox and solstices 24 hr. transients. The results have been statistically processed and compared with test data and correlation analysis in order to provide a reliable background for thermal control design and verification of future similar telecommunication satellites.
Meta TagsDetails
DOI
https://doi.org/10.4271/951749
Pages
8
Citation
Sacchi, E., Asteggiano, C., and Torrisi, R., "Thermal Design, Testing and On-Orbit Performance of the Italsat Communication Satellites," SAE Technical Paper 951749, 1995, https://doi.org/10.4271/951749.
Additional Details
Publisher
Published
Jul 1, 1995
Product Code
951749
Content Type
Technical Paper
Language
English