CubeSat’s Deployable Solar Panel with Viscoelastic Multilayered Stiffener for Launch Vibration Attenuation

<div>The PSD acceleration responses of the solar panel with various numbers of interlaminated stiffeners.</div>

International Journal of Aerospace Engineering

Figure 4: CubeSat’s Deployable Solar Panel with Viscoelastic Multilayered Stiffener for Launch Vibration Attenuation 