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Effects of Solar Array Shadowing on the Power Capability of the Interim Control Module NASA Glenn Research Center

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Fincannon, H. James (Homer James), author.
Conference Name:
34th Intersociety Energy Conversion Engineering Conference (1999-08-02 : Vancouver, Canada)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1999
Summary:
The Interim Control Module (ICM) is being built by the US Naval Research Laboratory (NRL) for NASA as a propulsion module for the International Space Station (ISS). Originally developed as a spinning spacecraft used to move payloads to their final orbit, for ISS, the ICM will be in a fixed orientation and location for long periods resulting in substantial solar panel shadowing. This paper describes the methods used to determine the incident energy on the ICM solar panels and the power capability of the electric power system (EPS). Applying this methodology has resulted in analyses and assessments used to identify ICM early design changes/options, placement and orientations that enable successful operation of the EPS under a wide variety of anticipated conditions
Notes:
Vendor supplied data
Publisher Number:
1999-01-2432
Access Restriction:
Restricted for use by site license

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