Accession Number:

AD0852658

Title:

Factory Acceptance Testing of Missile 66E.

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Report Date:

1961-11-20

Abstract:

Before conducting the missile composite checkout, successful performance of each individual system installed on the missile must be determined. The following is a list of the procedures used for acceptance testing of each system Electrical system Flight control system Inertial guidance system Instrumentation range safety system Propellant utilization system and Propulsion system. Author

Pages:

0049

Descriptors:

Identifiers:

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File Size:

0.00MB

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