SSC03-XI-04 Relative Navigation, Microdischarge Plasma Thruster, and Distributed Communications Experiments on the FASTRAC Mission

Abstract. Enabling technologies for nanosatellite formations will be demonstrated under the Formation Autonomy Spacecraft with Thrust, Relnav, Attitude, and Crosslink (FASTRAC) program. Two °ight-ready nanosatellites will be designed, fabricated, integrated, and tested during the two year design period. Three speci¯c new and innovative technologies which will be demonstrated during the mission are Relative Navigation, Plasma Microthrusters, and Distributed Communications. A sensor set consisting of Global Positioning System (GPS) receiver, magnetometer, and MEMS Inertial Measurement Unit (IMU) will be used to determine position and coarse attitude. Using a radio crosslink, the two satellites will exchange state vector information and perform sub-meter level accuracy relative navigation. Each satellite will also contain a Microdischarge Plasma Thruster (MPT) developed at UT-Austin. This innovative device is capable of generating low-thrust, high-e±ciency propulsion at low power levels using microdischarge plasmas. The ability of the MPT to extend the life of the orbit will be determined by monitoring the orbit decay rates of the two vehicles as well as the MEMS IMU. A distributed tracking network with multiple university partners will be utilized to track the low Earth orbit satellites. Amateur radio experimenters, high schools, universities, and other interested parties will be encouraged to record telemetry from the satellites and report their data to a project web site for processing. Although the main purpose of the mission is technology demonstration, science goals will also be pursued. These include post-processing sensor measurements to determine satellite drag, as well as Earth atmospheric and magnetospheric studies