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An Emergency Helium Bubbling Control System for the Prevention of Geysering in the Lox Suction Lines of S-ICAn emergency helium bubbling system was devised for geyser suppression in the LOX suction lines of S-IC . Flight model pressure and temperature transducers were compared to more accurate transducers to determine the best sensor configuration. Transducers were electronically simulated to calibrate the circuit design. A development system was tested for feasibility on a full- scale LOX flow line test facility.
Document ID
19650014190
Acquisition Source
Marshall Space Flight Center
Document Type
Other - 19650014190
Authors
James A Power (Marshall Space Flight Center Redstone Arsenal, United States)
A Turel (BROWN ENG. CO.)
Date Acquired
August 2, 2013
Publication Date
March 1, 1965
Subject Category
Auxiliary Systems
Report/Patent Number
N56-23791
Accession Number
65N23791
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LIQUID OXYGEN /LOX/
CONTROL SYSTEM
SATURN LAUNCH VEHICLE
HELIUM
BUBBLE
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