Stand-alone interplanetary CubeSats require primary propulsion systems for orbit maneuvering and precise trajectory control. The current work focuses on the design and performance characterization of the combined chemical–electric propulsion systems that shall enable a stand-alone 16U CubeSat mission on a hybrid high-thrust–low-thrust trajectory from a supersynchronous geostationary transfer orbit to a circular orbit about Mars. The high-thrust chemical propulsion is used to escape Earth and to initiate stabilization at Mars. The low-thrust electric propulsion is used in heliocentric transfer, ballistic capture, and circularization. For chemical propulsion, design and performance characteristics of a monopropellant thruster and feed system using ADN-based FLP-106 propellant are presented. For electric propulsion, a performance model of an iodine-propelled inductively coupled miniature radiofrequency ion thruster is implemented to calculate the variation of thrust, specific impulse, and efficiency with input power. A power-constrained low-thrust trajectory optimization using the thruster performance model is pursued to calculate the transfer time, Δ V , and the required propellant mass for fuel-optimal and time-optimal transfers. Overall, the combined chemical–electric systems yield a feasible propulsion solution for stand-alone CubeSat missions to Mars that balances propellant mass and transfer time.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Combined Chemical–Electric Propulsion for a Stand-Alone Mars CubeSat


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    2019-08-12


    Format / Umfang :

    15 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    SYSTEMS DESIGN OF MARIO: A STAND-ALONE 16U CUBESAT TO MARS

    Mani, Karthik Venkatesh / Casado, Alvaro Sanz / Franzese, Vittorio et al. | TIBKAT | 2020


    Staging of electric propulsion systems: Enabling an interplanetary Cubesat

    Krejci, David / Jenkins, Marco Gomez / Lozano, Paulo | Elsevier | 2019


    Magnetic properties of a 3U CubeSat with electric propulsion

    Treberspurg, Wolfgang / Stren, Andreas / Kügler, Holger et al. | Elsevier | 2023


    CubeSat Propulsion Using Electrospray Thrusters

    Roy, T. / Hruby, V. / Rosenblad, N. et al. | British Library Conference Proceedings | 2009