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  • Protection against micrometeoroid impacts in GEO satellites using aluminium-based self-healing material aided by accessible thermal energy

    Paper number

    IAC-20,C2,6,13,x60321

    Author

    Mr. Sanjay A, India, R V College of Engineering, Bengaluru

    Coauthor

    Mr. Kunal Bavikar, India, R V College of Engineering, Bengaluru

    Coauthor

    Mr. Maneesh M, India, R V College of Engineering, Bengaluru

    Coauthor

    Mr. Chathura G R, India, R V College of Engineering, Bengaluru

    Year

    2020

    Abstract
    With increasing bounds of space exploration, emerge new challenges; micrometeoroid impacts being one among them, becomes a liability to the overall mission criticality by inducing microcracks. Prolonged exposure to these impacts results in the coalescence of induced microcracks, ultimately leading to catastrophic failure before mission accomplishment. Space vessels being very much susceptible to these impacts require counter measures.
    
     This paper focusses on protecting Geosynchronous satellites against hypervelocity micrometeoroid impacts using self-healing material. The self-healing material is aluminium matrix composite reinforced with microcapsules containing healing agent. The healing agent is an aluminium-based liquid polymer engineered to harden as it fills the microcracks by using available thermal energy, mainly solar radiation. It is also designed to be stable at operating temperatures of the satellite structure. The structural properties of the self-healing material are studied before and after healing using which the healing efficiency is determined. Also, a comparison is made between the properties of the self-healing material and conventional materials (Aluminium Alloys).
    
    Further, the behaviour of self-healed material subjected to micrometeoroid impact is simulated using Finite Element Method (FEM) solver and the flow of healing agent into cracks is simulated using Computational Fluid Dynamics (CFD) analysis. Ultimately, this material can be used to replace the conventional materials that protect the satellite structure against micrometeoroid impacts as it self-heals without additional energy requirements with enhanced resistance to impacts.
    Abstract document

    IAC-20,C2,6,13,x60321.brief.pdf

    Manuscript document

    IAC-20,C2,6,13,x60321.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.