Accession Number : AD0842799

Title :   Electrical Connector, Separation Force, Evaluation Test.

Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s) : Hughey, L. R.

Report Date : 14 SEP 1960

Pagination or Media Count : 11

Abstract : The object of the test was to determine the forces required to unlock and disengage two electrical connectors. The connectors form a part of the electrical disconnect system between the Atlas and Centaur missile stages. (Author)

Descriptors :   (*ELECTRIC CONNECTORS, SEPARATION), (*LAUNCH VEHICLES, STAGING), FORCE(MECHANICS), TENSILE PROPERTIES, MISALIGNMENT, COLD WEATHER TESTS, INSTRUMENTATION, HUMIDITY, ACCEPTABILITY.

Subject Categories : Electrical and Electronic Equipment
      Ground Support Sys & Facil For Space Vehicles

Distribution Statement : APPROVED FOR PUBLIC RELEASE