Accession Number : AD0844180
Title : Evaluation Test of Liquid Oxygen Topping Line System Convair Drawing No. 27-21516,
Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA
Personal Author(s) : Palosaari, C. A.
Report Date : 27 APR 1961
Pagination or Media Count : 23
Abstract : This report describes tests performed on topping lines. The object of this was to determine if the re-designed liquid oxygen topping line would meet missile requirements. The topping line assembly was subjected to the Proof Pressure, Vibration, and Burst Tests as outlined in the procedure. The operation satisfied all design requirements. (Author)
Descriptors : (*PROPELLANT TANKS, PROPELLANT TRANSFER), (*PIPES, PERFORMANCE(ENGINEERING)), PRESSURIZATION, VIBRATION, RESONANT FREQUENCY, RUPTURE, FAILURE(MECHANICS), TOLERANCES(MECHANICS), JIGS, CLAMPS, CHECK VALVES, LIQUID ROCKET OXIDIZERS.
Subject Categories : Guided Missile Launching and Basing Support
Distribution Statement : APPROVED FOR PUBLIC RELEASE