Accession Number:

AD0852655

Title:

Factory Acceptance Testing of Missile 14F.

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Report Date:

1961-11-29

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 Atlas optical beacon system Azusa system Electrical system Flight control system Inertial guidance system Instrumentation beacon system Propellant utilization system Propulsion system Range safety command system and Telemetry system. Author

Pages:

0086

Descriptors:

Identifiers:

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File Size:

0.00MB

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