Accession Number : AD0843524
Title : Liquid Oxygen Pressure Loss Phase I and II,
Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA
Personal Author(s) : LaBerge, P. R.
Report Date : 12 MAY 1961
Pagination or Media Count : 18
Abstract : The pressure loss in the Centaur liquid oxygen system is a factor in the determination of the net positive suction head available to the turbopumps. The purpose of the tests is to determine the pressure loss in the Oxidizer Main Supply Duct (55-21504) while flowing liquid oxygen at various flow rates. (Author)
Descriptors : (*LAUNCH VEHICLES, PROPELLANT TANKS), (*FUEL SYSTEMS, PRESSURIZATION), OXYGEN, LIQUEFIED GASES, PRESSURE, OPERATION, TURBOPUMPS, SIMULATION, LIQUID ROCKET OXIDIZERS.
Subject Categories : Liquid Rocket Propellants
Ground Support Sys & Facil For Space Vehicles
Distribution Statement : APPROVED FOR PUBLIC RELEASE