Conventional spacecraft power system components are typically ill-suited to small satellites of less than approximately 300 kg total dry mass. In this paper the unique challenges of small satellite power systems are discussed. The development programs at the Air Force Research Laboratory which address these unique needs are presented.
Enabling Power Technologies for Small Satellites
Seventh International Conference and Exposition on Engineering, Construction, Operations, and Business in Space ; 2000 ; Albuquerque, New Mexico, United States
Space 2000 ; 530-536
2000-02-18
Conference paper
Electronic Resource
English
Enabling Power Technologies for Small Satellites
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