NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Program to design, fabricate, test, and deliver a thermal control-mixing control device, phase 1The development of a sensor capable of detecting temperature changes as a function of viscosity changes, was completed. This type of sensor, consisting of an orifice bridge circuit, resulted in a device with a threshold above internally generated noise of 0.8C (1.5F). Data were obtained using a noise free Freon source provided by an air pressurized bladder. Tests conducted to operate the sensor from a typical Freon centrifugal pump system employing an air bubble accumulator for noise attentuation disclosed the sensor could be used only to sense temperature changes greater than 3.3C (6F) because of the excessively noisy output. This is attributed to the high frequency-pressure fluctuations in the Freon supply to the sensor.
Document ID
19750025301
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Thurston, T. S.
(AiResearch Mfg. Co. Phoenix, AZ, United States)
Haley, S. W.
(AiResearch Mfg. Co. Phoenix, AZ, United States)
Date Acquired
September 3, 2013
Publication Date
September 16, 1975
Subject Category
Instrumentation And Photography
Report/Patent Number
PR-6
NASA-CR-143987
AIRESEARCH-75-410939(6)
Report Number: PR-6
Report Number: NASA-CR-143987
Report Number: AIRESEARCH-75-410939(6)
Accession Number
75N33374
Funding Number(s)
CONTRACT_GRANT: NAS8-31289
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available