Accession Number:

AD0844032

Title:

Error Demodulator Output Signal Hysteresis on Production 'E' Series Propellant Utilization Sets,

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s):

Report Date:

1961-05-29

Pagination or Media Count:

28.0

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

Subject Categories:

  • Electrical and Electronic Equipment
  • Surface-Launched Guided Missiles

Distribution Statement:

APPROVED FOR PUBLIC RELEASE