Abstract This paper regards small/midsize square sails on which a field of wrinkles appears owing to the necessary sail-membrane operations before and during the deployment. We collected a large amount of data in our laboratory. Many ten thousands of measurements had been statistically processed for characterizing some sail’s sampled membranes consisting of aluminized-polyimide layers ( 2.5 + 0.1 ) μ m thin, and loaded at vertices. Such samples have exhibited area and orientation alterations, as a whole, which can affect the propulsive acceleration of a sailcraft. Wrinkled-sail orientation has been given a thrust-specialized meaning for trajectory computation. Three-dimensional heliocentric minimum-time orbit transfer between Earth and Mercury orbits had been investigated. This had resulted in wrinkled-sail sailcraft moving on trajectories remarkably different from those ones of the corresponding ideal unwrinkled-sail sailcraft. Nevertheless, at least in the current framework, the most important result is that sail-wrinkled sailcraft’s interplanetary trajectories could be optimized without resorting to stochastic differential equations.


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    Titel :

    Wrinkling analysis of solar-photon sails


    Beteiligte:

    Erschienen in:

    Advances in Space Research ; 67 , 9 ; 2669-2687


    Erscheinungsdatum :

    2020-07-10


    Format / Umfang :

    19 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





    Corrigendum to “Wrinkling analysis of solar-photon sails” [Adv. Space Res. 67(9) (2021) 2669–2687]

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