Accession Number : AD0843153
Title : Study - Programming LOX Tank Pressure by Controlling the Regulator Sensing Line Pressure.
Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA
Personal Author(s) : Diedrich, E. C.
Report Date : 11 AUG 1961
Pagination or Media Count : 26
Abstract : The objective of this test was to investigate methods of programming a LOX tank airborne regulator so that a 26.0 psid maximum tank pressure would be maintained during the first twenty seconds of powered flight, and a 31.0 psid maximum pressure would be maintained during the remainder of the flight. (Author)
Descriptors : (*LAUNCH VEHICLES, PROPELLANT CONTROL), (*PROPELLANT TANKS, PRESSURIZATION), LIQUID ROCKET OXIDIZERS, PRESSURE REGULATORS, DETECTORS, BULKHEADS, BLEED SYSTEMS, TEST METHODS.
Subject Categories : Test Facilities, Equipment and Methods
Liquid Rocket Propellants
Ground Support Sys & Facil For Space Vehicles
Distribution Statement : APPROVED FOR PUBLIC RELEASE