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

Table 5

Estimated dynamic displacement of solar panels in vibration loads.

Test	Solar panel	Max. displacement (mm)
Sine vibration	w/o stiffener	0.49
	with 3 layers of stiffener	0.12
	with 5 layers of stiffener	0.05
Random vibration	w/o stiffener	1.39
	with 3 layers of stiffener	0.13
	with 5 layers of stiffener	0.04