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