International Journal of Aerospace Engineering / 2019 / Article / Tab 2

Research Article

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

Table 2

Mass budget of 6 U solar panel module.

ItemMass (g)

PCB panel with solar cells450
Stiffeners (3EA)110
Torsional hinges (2EA)25
Burn wire triggering HRM20
Mechanical parts (screws and nuts)20

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