The Propulsion System and Orbit Maneuver Integration in CubeSats project aims to solve the challenges of integrating a micro electric propulsion system on a CubeSat in order to perform orbital maneuvers and control attitude. This represents a fundamentally new capability for CubeSats, which typically do not contain propulsion systems and cannot maneuver far beyond their initial orbits.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Propulsion System and Orbit Maneuver Integration in CubeSats: Trajectory Control Strategies Using Micro Ion Propulsion


    Contributors:
    Hudson J. (author) / Martinez A. (author) / Petro A. (author)

    Publication date :

    2015


    Size :

    2 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





    Propulsion for CubeSats

    Lemmer, Kristina | Online Contents | 2017


    Propulsion for CubeSats

    Lemmer, Kristina | Elsevier | 2017


    Hybrid Propulsion for CubeSats

    Jens, Elizabeth | NTRS | 2016


    Hydrazine Propulsion Module for CubeSats

    Schmuland, D. / Masse, R. / Sota, C. et al. | British Library Conference Proceedings | 2011