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Constant Resistance Point Sensing for Propellant Gaging Systems

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Seeley, Eugene B., author.
Conference Name:
SAE World Congress & Exhibition (1964-01-01 : Detroit, Michigan, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1964
Summary:
A recently developed heated wire point liquid level detection system for use in cryogenic and other rocket propellants is described. Safety features include very low transducer element temperature in explosive gas mixtures, short circuit current limit below ignition thresholds, and remote checkout. Performance features include fast response, excellent interface resolution, and low power consumption. The controller maintains the level transducer element at nearly constant temperature in the varying thermal environment, and can differentiate liquid from gas by observation of the power dissipated. Application of the constant resistance control mode to both temperature control and direct measurement of fluid film heat transfer coefficients are considered
Notes:
Vendor supplied data
Publisher Number:
640485
Access Restriction:
Restricted for use by site license

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