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Galileo probe battery systems designNASA's Galileo mission to Jupiter will consist of a Jovian orbiter and an atmospheric entry probe. The power for the probe will be derived from two primary power sources. The main source is composed of three Li-SO2 battery modules containing 13 D-size cell strings per module. These are required to retain capacity for 7.5 years, support a 150 day clock, and a 7 hour mission sequence of increasing loads from 0.15 to 9.5 amperes for the last 30 minutes. This main power source is supplemented by two thermal batteries (CaCrO4-Ca) for use in firing the pyrotechnic initiators during the atmospheric staging events. This paper describes design development and testing of these batteries at the system level.
Document ID
19870030822
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Dagarin, B. P.
(Hughes Aircraft Co. El Segundo, CA, United States)
Van Ess, J. S.
(NASA Ames Research Center Moffett Field, CA, United States)
Marcoux, L. S.
(BTC Engineering, Ltd. North Vancouver, Canada)
Date Acquired
August 13, 2013
Publication Date
January 1, 1986
Subject Category
Spacecraft Propulsion And Power
Accession Number
87A18096
Funding Number(s)
CONTRACT_GRANT: NAS2-10000
Distribution Limits
Public
Copyright
Other

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