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

Table 2

Mass budget of the demonstration model of the mechanism.

Item	Mass (g)
Primary PCB	12.8
Secondary PCB with burn resistor (4EA)	1
Brackets (4EA)	2.8
Guide pins (12EA)	1.8
Total	18.4