Abstract The structural stability of a lightsail under the intense laser flux necessary for interstellar flight is studied analytically and numerically. A sinusoidal perturbation is introduced into a two-dimensional thin-film sail to determine if the sail remains stable or if the perturbations grow in amplitude. A perfectly reflective sail material that gives specular reflection of the laser illumination is assumed in determining the resulting loading on the sail, although other reflection models can be incorporated as well. The quasi-static solution of the critical point between shape stability and instability is found by equating the bending moments induced on the sail due to radiation pressure with the restoring moments caused by the strength of the sail material and the tension applied at the edges of the sail. From this quasi-static solution, analytical expressions for the critical value of elastic modulus and boundary tension magnitude are found as a function of sail properties (e.g., thickness) and the amplitude and wave number of the initial sinusoidal perturbation. These same expressions are also derived from a more formal variational energy (virtual work) approach. A numerical model of the complete lightsail dynamics is developed by discretizing the lightsail into rectangular finite elements. By introducing torsional and rectilinear springs between the elements into the numerical model, a hierarchy of models is produced that can incorporate the effects of bending and applied tension. The numerical models permit the transient dynamics of a perturbed lightsail to be compared to the analytic results of the quasi-static analysis, visualized as stability maps that show the rate of perturbation growth as a function of sail thickness, elastic modulus, and applied tension. The analytic theory is able to correctly predict the stability boundary found in the numerical simulations. The stiffness required to make a thin lightsail stable against uncontrolled perturbation growth appears to be unfeasible for known materials, however, a relatively modest tensioning of the sail (e.g., via an inflatable structure or spinning of the sail) is able to maintain the sail shape under all wavelengths and amplitudes of perturbations.

    Highlights The shape of a flat lightsail was perturbed to test its resistance to deformation. Quasi-static analytical expressions were developed for the critical stability point. Dynamics of the perturbed lightsail was studied using numerical models. Analytical expressions predict the stability boundary seen in numerical simulations. Sail tensioning, not increasing material stiffness, is a method to obtain stability.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Structural stability of a lightsail for laser-driven interstellar flight


    Beteiligte:

    Erschienen in:

    Acta Astronautica ; 201 ; 376-393


    Erscheinungsdatum :

    2022-09-01


    Format / Umfang :

    18 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    LASER LIGHTSAIL SPACECRAFT FOR INTERSTELLAR EXPLORATION

    Atwater, Harry / Schalkwyk, James | TIBKAT | 2020


    STRUCTURAL STABILITY OF A LIGHTSAIL FOR LASER-DRIVEN PROPULSION

    Savu, Dan-Cornelius / Higgins, Andrew J. | TIBKAT | 2020


    Dust Grain Damage to Interstellar Laser-Pushed Lightsail

    James T. Early / Richard A. London | AIAA | 2000


    Structural Stability of a Lightsail for Laser-Driven Propulsion

    Savu, Dan-Cornelius / Higgins, Andrew J. | AIAA | 2020


    INTERACTION OF INTERPLANETARY DUST WITH A LASER-DRIVEN LIGHTSAIL DURING ACCELERATION

    Higgins, Andrew / Azmanska, Monika / Kaur, Navneet et al. | TIBKAT | 2020