Accession Number:

AD0852189

Title:

Factory Acceptance Testing of Missile 30F.

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s):

Report Date:

1961-11-01

Pagination or Media Count:

34.0

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

Subject Categories:

  • Surface-Launched Guided Missiles

Distribution Statement:

APPROVED FOR PUBLIC RELEASE