F-Sat is a standard spacecraft bus which will support future LMSC programs, both commercial and government. The F-Sat bus has been designed with the adaptability to satisfy any applications with medium-weight payloads. This paper discusses F-Sat's design and a recently completed test which demonstrated the integration of flight electronics with attitude determination and control system sensors and actuators. With the successful completion of this demonstration. F-Sat has taken one more step toward realizing the goal of low cost access to space.
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