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Device disconnects several couplings simultaneouslyActuator 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.
Document ID
19650000161
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Forsythe, A. K.
Date Acquired
August 2, 2013
Publication Date
June 1, 1965
Subject Category
Mechanics
Report/Patent Number
JPL-226
Accession Number
65B10163
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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