Accession Number:

AD0852239

Title:

Factory Acceptance Testing of Missile 57E.

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Report Date:

1961-07-03

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 Propellant utilization system and Propulsion system.

Pages:

0037

Identifiers:

Subject Categories:

Communities Of Interest:

File Size:

0.00MB

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