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

<div>Configuration of a pogo pin-type holding and release mechanism proposed in the study: (a) overall configuration, (b) holding state, and (c) release state.</div>

International Journal of Aerospace Engineering

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Figure 3

Figure 3: Experimental Investigation on the Feasibility of Using Spring-Loaded Pogo Pin as a Holding and Release Mechanism for CubeSat’s Deployable Solar Panels 

Figure 3 | Experimental Investigation on the Feasibility of Using Spring-Loaded Pogo Pin as a Holding and Release Mechanism for CubeSat’s Deployable Solar Panels 