Accession Number : AD0843161
Title : Control of Chilldown and Pressure Rise in SF-1 Cruiser Tank and Transfer Line.
Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA
Personal Author(s) : Tengan, S.
Report Date : 03 APR 1961
Pagination or Media Count : 12
Abstract : The objective of this test is to establish an optimum chilldown procedure for the SF-1 Transfer Line and Cruiser Tank, utilizing a minimum amount of SF-1 and the minimum time without exceeding the safe missile fuel tank operating pressure (11 psig) and boiloff valve capability. (Author)
Descriptors : (*LAUNCH VEHICLES, PROPELLANT TRANSFER), CONTROL SYSTEMS, PROPELLANT TANKS, PIPES, FUEL SYSTEMS, PRESSURIZATION, GUIDED MISSILE SAFETY, STANDARDIZATION.
Subject Categories : Liquid Rocket Propellants
Ground Support Sys & Facil For Space Vehicles
Distribution Statement : APPROVED FOR PUBLIC RELEASE