Accession Number : AD0844521
Title : Propellant Tanking Overflow Tube,
Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA
Personal Author(s) : LaBerge, P. R.
Report Date : 20 JUN 1961
Pagination or Media Count : 11
Abstract : The objective of the test was to utilize the fuel standpipe and the oxidizer standpipe (overflow tubes) to accurately indicate and preserve the 100% station level during propellant loading. (Author)
Descriptors : (*PROPELLANT TRANSFER, LIQUID LEVEL CONTROL), LAUNCH VEHICLES, PIPES, VALVES, LIQUID ROCKET PROPELLANTS.
Subject Categories : Liquid Rocket Propellants
Ground Support Sys & Facil For Space Vehicles
Distribution Statement : APPROVED FOR PUBLIC RELEASE