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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
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2020
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Article
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Tab 2
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Research Article
Experimental Validation of a Highly Damped Deployable Solar Panel Module with a Pogo Pin-Based Burn Wire Triggering Release Mechanism
Table 2
Mass budget of the demonstration model of the 3 U solar panel module.
Items
Mass (g)
PCB panel
93
Five layers of the PCB stiffener
45
Five layers of the adhesive tape
3
Pogo pin-based HRM
6
Torsional hinge
11
Total
158