Factory Acceptance Testing of Missile 118D.
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; Guidance system; Instrumentation range safety system; Propellant utilization system; and Propulsion system. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jul 28, 1961
- Accession Number
- AD0852233
Entities
Organizations
- General Dynamics