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.

Subject Categories:

  • Test Facilities, Equipment and Methods
  • Solid Rocket Propellants

Distribution Statement:

APPROVED FOR PUBLIC RELEASE