Non-explosive Low-shock Separation Device for small satellite

In this paper, we report a non-explosive separation device for a small satellite which utilize a shape memory alloy actuator. Based on previous research, we try to increase the reliability of the proposed device by changing some components. It enables the proposed device to activate under high preload. Also, we confirm it generates low shock which is main advantage of non-explosive separation device. Finally, vibration test which mimics launching environment and thermal vacuum test which mimics space

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Non-explosive Low-shock Separation Device for small satellite

Cited by 2 publications

References 1 publication

Ejection Mechanism Design for Space-net-based Active Debris Removal

Ejection Mechanism Design for Space-net-based Active Debris Removal

Performance evaluation on the separation device activated by shape memory alloy actuator

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