NASA NTRS · 19650000161
Device disconnects several couplings simultaneously
Abstract
Actuator assembly disconnects electric cable and fluid-line coupling from a rocket. The disconnector incorporates interconnected hydraulic cylinders which effect an equal and simultaneous displacement of pistons upon admission of compressed air through a solenoid control valve.
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Forsythe, A. K.. 1965-06-01. Device disconnects several couplings simultaneously. https://ntrs.nasa.gov/citations/19650000161
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