International Journal of Aerospace Engineering / 2019 / Article / Tab 4

Research Article

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

Table 4

Low level sine sweep (LLSS) test results.

TestAxis1st eigenfrequency (Hz)Difference (%)

Sine vibrationXBefore324.060.68
After326.26
YBefore378.90.32
After381.27
ZBefore73.410.23
After73.24

Random vibrationXBefore326.452.48
After318.35
YBefore377.80.73
After380.54
ZBefore73.245.42
After69.27

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