Factory Acceptance Testing of Missile 40E.

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: 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.

Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1961
Accession Number
AD0852235

Entities

Organizations

  • General Dynamics

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Control Systems
  • Flight Control Systems
  • Guidance
  • Inertial Navigation
  • Inertial Navigation Systems
  • Instrumentation
  • Navigation
  • Propulsion Systems
  • Range Safety

Fields of Study

  • Physics

Readers

  • Aerospace Test and Evaluation
  • Inertial Navigation Systems.