International Journal of Aerospace Engineering / 2019 / Article / Tab 3

Research Article

Development of 6 U CubeSat’s Deployable Solar Panel with Burn Wire Triggering Holding and Release Mechanism

Table 3

Summary of qualification test specifications.
(a) Sinusoidal vibration test

Frequency (Hz)Amplitude (g)Sweep rate (oct/min)

51.32
82.5
1002.5

(b) Random vibration test

Frequency (Hz)Amplitude (g)Overall Test duration (min)

200.02614.12
500.16
8000.16
20000.026

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