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Evaluation of Viking Lander barometric pressure sensorVariable reluctance type pressure sensors were evaluated to determine their performance characteristics related to Viking Mission environment levels. Static calibrations were performed throughout the evaluation over the full range of the sensors using two point contact manometer standards. From the beginning of the evaluation to the end of the evaluation, the zero shift in the two sensors was within 0.5 percent, and the sensitivity shift was 0.05 percent. The maximum thermal zero coefficient exhibited by the sensors was 0.032 percent over the temperature range of -28.89 C to 71.11 C. The evaluation results indicated that the sensors are capable of making high accuracy pressure measurements while being exposed to the conditions mentioned.
Document ID
19770013216
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Mitchell, M.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
March 1, 1977
Subject Category
Spacecraft Instrumentation
Report/Patent Number
NASA-TM-X-74020
Report Number: NASA-TM-X-74020
Accession Number
77N20160
Funding Number(s)
PROJECT: RTOP 815-10-00-00-06
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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