Accession Number:

AD0852232

Title:

Factory Acceptance Testing of Missile 93D.

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Report Date:

1961-09-25

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 Abort sensing and implementation system Azusa system Electrical system Flight control system Guidance system Propellant utilization system Propulsion system Range safety command system and Telemetry system. Author

Supplementary Note:

Report on Project Mercury.

Pages:

0091

Descriptors:

Identifiers:

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Communities Of Interest:

File Size:

0.00MB

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