Accession Number : AD0842173
Title : HIGH RATE FILL STUDIES E-SERIES FUEL,
Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA
Personal Author(s) : Calimbas, A.
Report Date : 08 AUG 1960
Pagination or Media Count : 24
Abstract : This report defines tests performed to determine the following: the flow characteristics (liquid trajectory) of the fill jet issuing from the fuel staging disconnect during fill using water as the flow medium, the loads upon the tank and the effect of the jet impingement on the missile internal structure, pressure losses and flow rates in the fill plumbing during tanking, and the imposed stresses on the fill duct during filling operations. (Author)
Descriptors : *PROPELLANT TRANSFER), (*SURFACE TO SURFACE MISSILES, (*PROPELLANT TANKS, LOADS(FORCES)), FLUID FLOW, TRAJECTORIES, INTERFACES, IMPACT, PRESSURE, FORCE(MECHANICS), STRAIN(MECHANICS), STRESSES, GROUND SUPPORT EQUIPMENT.
Subject Categories : Surface-launched Guided Missiles
Liquid Propellant Rocket Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE