The CANSAT design, a simple and small scale of a satellite, is an experience for preparing for the design of a Life cycle of the space project. In this paper, the process of design and construction of ARTA CanSat, which is participated in the scientific-exploratory class of international competition in CANSAT Iran, has been written. The operation scenario is that an automatic scanner system, lands after releasing from 300 meters above ground level with using a recovery subsystem (parachute), which is controlled its downfall and landing position by the parachute controller system. During the descent, the data is transmitted by the sensors and sent to the ground station. After touchdown, the Hotwire system's operates and separates the parachute from the Rover section; Then CanSat with the moving on the ground by using the simpler section embedded underneath the structure, performing excavation while moving to the target point. Throughout the mission, the health of the biological payload is preserved.


    Access

    Download


    Export, share and cite



    Title :

    The presentation of the ARTA CanSat design and construction process at the CANSAT International Competition in Iran




    Publication date :

    2020




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    Unknown




    Model satellite design for CanSat Competition

    Bulut, Sultan Nur / Gul, Mahircan / Beker, Can et al. | IEEE | 2013


    Norwegian CanSat Competition Pilot

    Wang, T. / Vandeberg, R. / European Space Agency | British Library Conference Proceedings | 2009


    Small space can: CanSat

    Soyer, S. | IEEE | 2011


    CanSat Teacher Training Course

    Gansmoe, T. / Grande, J. / European Space Agency | British Library Conference Proceedings | 2013


    Cansat Project 2002

    Ikeda, Mitsuhisa / Jang, Jae-Hyeuk / Wakana, Hiromitsu | AIAA | 2003