Experimental Investigation on the Feasibility of Using Spring-Loaded Pogo Pin as a Holding and Release Mechanism for CubeSat’s Deployable Solar Panels

<div>MEMS-based solid propellant thruster and its control board with spring-loaded pogo pin [<a href="/journals/ijae/2018/4854656/#B22">22</a>].</div>

International Journal of Aerospace Engineering

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Figure 2: Experimental Investigation on the Feasibility of Using Spring-Loaded Pogo Pin as a Holding and Release Mechanism for CubeSat’s Deployable Solar Panels 

Figure 2 | Experimental Investigation on the Feasibility of Using Spring-Loaded Pogo Pin as a Holding and Release Mechanism for CubeSat’s Deployable Solar Panels 