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Thin film strain transducerPrevious attempts to develop an appropriate sensor for measuring the stress or strain of high altitude balloons during flight are reviewed as well as the various conditions that must be met by such a device. The design, development and calibration of a transducer which promises to satisfy the necessary design constraints are described. The thin film strain transducer has a low effective modulus so as not to interfere with the strain that would naturally occur in the balloon. In addition, the transducer has a high sensitivity to longitudinal strain (7.216 mV/V/unit strain) which is constant for all temperature from room temperature to -80 C and all strains from 5 percent compression to 10 percent tensile strain. At the same time, the sensor is relatively insensitive (0.27 percent) to transverse forces. The device has a standard 350 ohm impedance which is compatible with available bridge balance, amplification and telemetry instrumentation now available for balloon flight. Recommendations are included for improved coatings to provide passive thermal control as well as model, tethered and full scale flight testing.
Document ID
19810011877
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Rand, J. L.
(Southwest Research Inst. San Antonio, TX, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1981
Subject Category
Instrumentation And Photography
Report/Patent Number
NASA-CR-156875
Report Number: NASA-CR-156875
Accession Number
81N20406
Funding Number(s)
CONTRACT_GRANT: NAS6-3077
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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