The purpose of this work is to describe the use of electrospray propulsion devices as miniaturized actuators for precise attitude control of small satellites, including CubeSats. Electrosprays are nonpressurized, passively fed, compact and fuel-efficient electric thrusters capable of producing impulse bits in the 10-6 N·s or lower, depending on the configuration. These characteristics have the potential to allow for long-term pointing in the arcsecond range or better with practically no jitter. Experimental work is performed on a magnetically levitated testbed in vacuum to demonstrate the actuation characteristics under nonoptimal control. It is found that, subject to a noisy attitude sensor and external perturbations, electrospray thrusters are capable of producing pointing accuracies around a given set point of 22 arcseconds 3Ï[function of] error during 10 h on a platform similar in size and mass to a 1U CubeSat. The implementation of such capabilities could complement or eliminate the need of reaction wheels and magnetorquers, especially in missions beyond low Earth orbit, while including propulsive capabilities for additional maneuverability in technology development or scientific missions.


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    Title :

    Electrospray Thrusters as Precise Attitude Control Actuators for Small Satellites




    Publication date :

    2016




    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    55.54 Flugführung
    Local classification TIB:    770/7040





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