The closure is for the exhaust nozzles of missiles of the Polaris type. The closure ejects when subjected to 130 p.s.i.a. The structure includes a Styrofoam plug, a cellulose acetate facing plate adhering to the plug and a diaphragm which extends across the facing of the plug and around the rim of the nozzle.
Bondless 'High Performance' Rocket Nozzle Closure
1966
1 pages
Report
No indication
English
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