Accession Number:

AD0852733

Title:

Factory Acceptance Testing of Missile 40F.

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Report Date:

1961-12-18

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. Author

Pages:

0035

Descriptors:

Identifiers:

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Communities Of Interest:

File Size:

0.00MB

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