Orifice Sizing and Component Evaluation for a Programmed LOX Tank Pressure on the Atlas/Agena Booster,
Abstract
The objective of the test was to evaluate the performance of the components and the plumbing configuration required to program the LOX tank pressure needed during the flight of the Atlas/Agena booster. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 19, 1962
- Accession Number
- AD0861341
Entities
People
- R. T. Spencer
Organizations
- General Dynamics