NASA'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.
Galileo probe battery systems design
Planung der Batteriesysteme fuer die Galileo-Sonde
1986
7 Seiten, 9 Bilder, 2 Tabellen
Conference paper
English
IEEE | 1996
|NTRS | 1997
|British Library Conference Proceedings | 1997
|Online Contents | 1996
|The Galileo probe Li/SO2 battery
Tema Archive | 1983
|