PROTOTYPE PROPELLANT-TESTING SYSTEM. PHASES 1 AND 2 - FEASIBILITY STUDY AND PRELIMINARY DESIGN
AEROJET-GENERAL CORP AZUSA CA
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The feasibility of constructing a test system for studying dynamic effects in liquid-propellant streams was examined and a prototype system was designed that is acceptable for use with storable, corrosive, or cryogenic fuels and oxidizers. Recommendations are made for on-stream analyzers suitable for the monitoring of a wide range of physical and bsequent tests.
- Test Facilities, Equipment and Methods
- Solid Rocket Propellants