XSM-65D AIG PROPELLANT UTILIZATION SYSTEM DESCRIPTION AND TEST PLAN,
Abstract
This document is provided to establish the test objectives required to perform a complete System Checkout of the Missileborne Propellant Utilization System. The method, by which the parameters are measured, and the capabilities required of the Checkout Equipment are described. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- May 22, 1959
- Accession Number
- AD0833162
Entities
People
- R. J. Bjorstrom
Organizations
- General Dynamics