Factory Acceptance Testing of Missile 18F.
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)
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 19, 1961
- Accession Number
- AD0852237
Entities
Organizations
- General Dynamics