Thermal Design and Analysis of the CERES Instrument for the EOS-AM Spacecraft

This paper describes the thermal design and analysis of the Clouds and the Earth's Radiant Energy System (CERES) instrument with emphasis on the detector thermal design. CERES has been selected as a payload on the Earth Observing System (EOS-AM-1) spacecraft which is the principle component of...

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Veröffentlicht in:	SAE transactions 1995-01, Vol.104, p.739-749
1. Verfasser:	Killough, Brian D.
Format:	Artikel
Sprache:	eng
Schlagworte:	Aluminum Bolometers Ceres Design Design analysis Radiators Spacecraft Spacecraft orbits Thermal analysis Time constants
Online-Zugang:	Volltext
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