Recent successes in the effort to miniaturize spacecraft components using M
EMS technology, integrated passive components, and low power electronics ha
ve driven the need for very low power, low profile, low mass micro-power so
urces for micro/nanospacecraft applications. Recent work at JPL has focused
upon developing thin film/micro-batteries compatible with temperature sens
itive substrates. A process to prepare crystalline LiCoO2 films with RF spu
ttering and moderate (< 700 degreesC) annealing temperature has been develo
ped. Thin film batteries with cathode films prepared with this process have
specific capacities approaching the practical limit for LiCoO2, with accep
table rate capabilities and discharge voltage profiles. Solid-state micro-s
cale batteries have also been fabricated with feature sizes on the order of
50 microns.