SECONDARY PRESSURE REGULATOR TEST.
Abstract
The purpose of this investigation was to evaluate a secondary pressure regulator for its suitability as a secondary or lockout regulator in the propellant pressurization system. The test requirements included; determination of leakage, lockout pressure, flow capacity and response to vibration and acceleration environments. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 28, 1958
- Accession Number
- AD0801715
Entities
People
- Jack Arct
Organizations
- Lockheed Martin Missiles and Space