Accession Number:
AD0297040
Title:
PROTOTYPE PROPELLANT-TESTING SYSTEM. PHASES 1 AND 2 - FEASIBILITY STUDY AND PRELIMINARY DESIGN
Descriptive Note:
Corporate Author:
AEROJET-GENERAL CORP AZUSA CA
Personal Author(s):
Report Date:
1963-02-01
Pagination or Media Count:
131.0
Abstract:
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.
Descriptors:
Subject Categories:
- Test Facilities, Equipment and Methods
- Solid Rocket Propellants