Experimental Validation of a Highly Damped Deployable Solar Panel Module with a Pogo Pin-Based Burn Wire Triggering Release Mechanism

Table 5

LLSS test results of the solar panels before and after full level vibration tests.

Test	Axis	Status	1^st eigenfrequency (Hz)	Difference (%)
Sine vibration	x	Before	471.58	0.45
		After	473.71
	y	Before	111.17	3.20
		After	107.72
	z	Before	54.83	0.46
		After	54.58
Random vibration	x	Before	471.58	0.45
		After	473.71
	y	Before	106.28	0.91
		After	105.32
	z	Before	55.33	2.31
		After	54.08