International Journal of Aerospace Engineering / 2019 / Article / Tab 2

Research Article

Development of Pogo Pin-Based Holding and Release Mechanism for Deployable Solar Panel of CubeSat

Table 2

Specifications of launch vibration test loads at qualification level.
(a) Sine vibration [18]

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

0 dB (full level)51.32
82.5
1002.5

(b) Random vibration [19]

LevelFrequency (Hz)Amplitude (g2/Hz)Duration (s)RMS acceleration

0 dB (full level)200.026012014.10 
500.1600
8000.1600
20000.0260

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