COMPARISON OF PERFORMANCES OF TWO HELIUM PRESSURIZATION REGULATORS UNDER 3600 PSI INLET PRESSURE CONDITIONS,
Abstract
The object of this test was to determine whether either, or both, of the test specimens would perform satisfactorily with an inlet pressure of 3600 psig which was 600 psig above the design inlet pressure. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 16, 1959
- Accession Number
- AD0800826
Entities
People
- F. D. D'alo
Organizations
- Lockheed Martin Missiles and Space