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

<div>Free-vibration test setup configuration of the solar panel in a thermal chamber.</div>

International Journal of Aerospace Engineering

Figure 6: CubeSat’s Deployable Solar Panel with Viscoelastic Multilayered Stiffener for Launch Vibration Attenuation 