Accession Number : AD0675720

Title :   PROPELLANT UTILIZATION DIFFERENTIAL RATIO SYSTEM USING STANDARD PRESSURE SENSORS,

Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CALIF

Personal Author(s) : Kennedy,N. H.

Report Date : 14 AUG 1961

Pagination or Media Count : 36

Abstract : A basic problem in Propellant Utilization is the achievement of a simple, reliable and rugged propellant sensor. This report describes a method of using inexpensive standard type pressure sensors to provide propellant mass ratio control. (Author)

Descriptors :   (*LIQUID PROPELLANT ROCKET ENGINES, LIQUID ROCKET PROPELLANTS), (*PROPELLANT CONTROL, DETECTORS), LAUNCH VEHICLES, LIQUID ROCKET FUELS, LIQUID ROCKET OXIDIZERS, LIQUID LEVEL CONTROL, PROPELLANT CONTROL, PROPELLANT TRANSFER, PROPELLANT TANKS, PRESSURE, ACCELERATION, CURVE FITTING, INSTRUMENTATION, CALIBRATION

Subject Categories : Liquid Rocket Propellants

Distribution Statement : APPROVED FOR PUBLIC RELEASE