NASA NTRS · 19760021191
Pin puller impact shock attenuation
Abstract
Design of a pin arresting mechanism for a pyrotechnically actuated pin puller is reviewed. The investigative approach is discussed and the impact shock test results for various candidate designs are presented. The selected pin arresting design reduced the peak value of the shock response spectrum by five to one.
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Auclair, G. F., Leonard, B. S., Robbins, R. E., Proffitt, W. L.. 1976-07-01. Pin puller impact shock attenuation. https://ntrs.nasa.gov/citations/19760021191
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