Error Demodulator Output Signal Hysteresis on Production 'E' Series Propellant Utilization Sets,
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)
Document Details
- Document Type
- Technical Report
- Publication Date
- May 29, 1961
- Accession Number
- AD0844032
Entities
People
- G. J. Kaleta
Organizations
- General Dynamics