Accession Number : AD0844032
Title : Error Demodulator Output Signal Hysteresis on Production 'E' Series Propellant Utilization Sets,
Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA
Personal Author(s) : Kaleta, G. J.
Report Date : 29 MAY 1961
Pagination or Media Count : 28
Abstract : The objective of the test was to gather data from a number of production 'E' series propellant utilization units, during factory calibration, in order to determine: (a) whether the error demodulator output signal hysteresis is random or systematic from set to set, and (b) the effect of a modified tip support in the liquid oxygen manometer on the zero pressure error demodulator output reading. (Author)
Descriptors : (*DEMODULATORS, HYSTERESIS), SIGNALS, LIQUID LEVEL CONTROL, LIQUID ROCKET PROPELLANTS, SURFACE TO SURFACE MISSILES, PRESSURE, MANOMETERS, VIBRATION, SOLENOIDS.
Subject Categories : Electrical and Electronic Equipment
Surface-launched Guided Missiles
Distribution Statement : APPROVED FOR PUBLIC RELEASE