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Hubble Space Telescope electrical power system modelThis paper describes one of the most comprehensive models ever developed for a spacecraft electrical power system (EPS). The model was developed for the Hubble Space Telescope (HST) to evaluate vehicle power system performance and to assist in scheduling maintenance and refurbishment missions by providing data needed to forecast EPS power and energy margins for the mission phases being planned. The EPS model requires a specific mission phase description as the input driver and uses a high granularity database to produce a multi-orbit power system performance report. The EPS model accurately predicts the power system response to various mission timelines over the entire operational life of the spacecraft.
Document ID
19890028004
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Baggett, Randy
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Miller, Jim
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Leisgang, Tom
(Lockheed Missiles and Space Co., Inc. Sunnyvale, CA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1988
Subject Category
Computer Programming And Software
Meeting Information
Meeting: 1988 IECEC
Location: Denver, CO
Country: United States
Start Date: July 31, 1988
End Date: August 5, 1988
Accession Number
89A15375
Distribution Limits
Public
Copyright
Other

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