Independent deep-space CubeSat missions require efficient propulsion systems capable of delivering several km/s of ΔV. The ion Electrospray Propulsion System under development at MIT's Space Propulsion Laboratory is a high ΔV propulsion system that is a promising technology for propulsion of independent deep-space CubeSat missions due to its mechanical simplicity and small form factor. However, current electrospray thrusters have demonstrated lifetimes up to an order of magnitude lower than the required firing time for a mission to a near-Earth asteroid starting from geostationary orbit. A stage-based concept is proposed where the propulsion system consists of a series of electrospray thruster arrays. When a set of thrusters reaches its lifetime limit, it is ejected from the spacecraft exposing new thrusters thereby increasing the overall lifetime of the propulsion system. Such a staging strategy is usually not practical for in-space thrusters. However, the compactness of micro-fabricated electrospray thrusters means that their contribution to the overall spacecraft mass and volume is small relative to other subsystems. Mechanisms required for this stage-based approach are proposed and demonstrated in a vacuum environment. In addition, missions to several near-Earth asteroids with orbital elements similar to those of Earth are analyzed with a particular focus on the escape trajectory. With a stage-based approach, independent deep-space CubeSat missions become feasible from a propulsion standpoint.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Stage-Based Electrospray Propulsion System for Deep-Space Exploration with CubeSats


    Contributors:


    Publication date :

    2019-03-01


    Size :

    6408755 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English





    Propulsion for CubeSats

    Lemmer, Kristina | Online Contents | 2017


    Electrospray Mission Modeling for CubeSats

    Hatch, A. / Black, J. / Utah State University; American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2013


    Hybrid Propulsion for CubeSats

    Jens, Elizabeth | NTRS | 2016