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  • Thermal deformation on laser retro-reflectors of LARES satellite

    Paper number

    IAC-15,C2,2,10,x30950

    Author

    Prof. Antonio Paolozzi, University of Rome “La Sapienza”, Italy

    Coauthor

    Prof. Ignazio Ciufolini, Università del Salento, Italy

    Coauthor

    Mr. Claudio Paris, University of Rome “La Sapienza”, Italy

    Coauthor

    Prof. Maurizio Parisse, University of Rome “La Sapienza”, Italy

    Year

    2015

    Abstract
    LARES is an Italian Space Agency satellite that was successfully put in orbit with the qualification launch of VEGA. The surface of the satellite is covered with 92 Cube Corner Reflectors (CCRs) that allow its precise positioning through the measurements of the International Laser Ranging Service. By measuring the time of flight of the laser pulses sent towards the satellite it is possible to reach ranging accuracies of few millimeters from the best stations. LARES is passive and as such it does not have thermal control. Thermal deformations of the CCRs can be calculated if power input, boundary conditions and thermal heat transfer parameters are known. The reflecting performances of CCRs are typically evaluated through the analysis of the Far Field Diffraction Pattern (FFDP) which provides information on the energy distribution, of the reflected laser pulse, on the ground. The CCR deformations can change the FFDP thus reducing the probability to have good laser returns to the station. Due to its particular CCR mounting system, that minimizes contact with the CCR, heat transfer of the CCR is mainly governed by radiation. It is therefore important to evaluate experimentally the solar absorptivity $\alpha_S$ and the  infrared emissivity $\varepsilon$. The paper will describe the experimental set-up, the numerical thermal model of the CCR and mounting system and the experimental  measurement of absorptivity and emissivity. The thermal model with the experimentally evaluated $\alpha_S$  and $\varepsilon$ will be used to calculate the deformation. It will finally be verified if those deformation are compatible with the Far Field Diffraction Pattern that will be experimentally acquired using a special optical circuit outside the thermal vacuum chamber.
    Abstract document

    IAC-15,C2,2,10,x30950.brief.pdf

    Manuscript document

    IAC-15,C2,2,10,x30950.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.