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

<div>1<sup>st</sup> eigenfrequency of the solar panels under various temperature conditions.</div>

International Journal of Aerospace Engineering

Figure 7: CubeSat’s Deployable Solar Panel with Viscoelastic Multilayered Stiffener for Launch Vibration Attenuation 