An Intelligent Strain Gauge with Debond Detection and Temperature Compensation

Metadata Updated: February 28, 2019

The harsh rocket propulsion test environment exposes any inadequacy associated with preexisting instrumentation technologies, can critically affect the collection of reliable test data, and justifies investigating any encountered data anomalies.  Novel concepts for improved system assessments are often conceived during the high scrutiny investigations by individuals with an in-depth knowledge from maintaining critical test operations.  The intelligent strain gauge concept developed for this project was conceived while performing these kinds of activities. Ordinary gauges are designed to provide test article data but they lack the ability to supply information concerning the gauge itself. Changes to the gauge bond integrity are observable in the thermal dissipation rate. A gauge is considered to be a "smart gauge" when it provides supplementary data relating Instrument attributes for performing diagnostic function or producing enhanced data.  Accordingly, a gauge with the ability to temporarily self-heat and monitor the rate at which the thermal dissipation occurs can indicate a gauge debond. This project developed novel strain gauge designs that enabled the detection of gauge debonding, and provided for temperature compensation of strain measurements. The improvement to the gauge increased instrument functionality and data collection capability. Two types of fully functional smart strain gauges capable of performing reliable and sensitive debond detection were successfully produced.  To improve instruments functionality in a harsh rocket propulsion test environment, this project developed an intelligent strain gauge.  The initial design for this project was a novel foil strain gauge with the capability to measure strain and temperature (Type 1).  The novel foil strain gauge pattern features the integration of a silicon-diode temperature sensor and a self-heating element. The silicon-diode sensor provides the gauge temperature for performing real-time temperature compensation algorithms. The silicon-diode temperature sensor was used in the initial gauge pattern due to its enhanced abilities, but after refinement, resistive temperature element was then embedded into a second gauge pattern (Type 2). Then, the debond detection function was tested by monitoring the temperature of the gauge while the gauge was heated and cooled. The temperature signature (rate of heating/cooling) from the gauge was analyzed for both bonded and debonded gauges. Finally, a small control circuit was created with the capability to self-execute a bond integrity check, and perform real-time temperature compensation was also added. By combining the control circuit with the special gauge the smart gauge was converted into a fully functioning intelligent sensor system.

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Public: This dataset is intended for public access and use. License: U.S. Government Work

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Metadata Created Date August 1, 2018
Metadata Updated Date February 28, 2019

Metadata Source

Harvested from NASA Data.json

Additional Metadata

Resource Type Dataset
Metadata Created Date August 1, 2018
Metadata Updated Date February 28, 2019
Publisher Space Technology Mission Directorate
Unique Identifier TECHPORT_10587
Maintainer Email
Public Access Level public
Bureau Code 026:00
Metadata Context
Metadata Catalog ID
Schema Version
Catalog Describedby
Harvest Object Id a8e6cb6e-af72-4d7a-b6d0-6aa9b586b8c0
Harvest Source Id 39e4ad2a-47ca-4507-8258-852babd0fd99
Harvest Source Title NASA Data.json
Data First Published 2012-10-01
Homepage URL
Data Last Modified 2018-07-19
Program Code 026:027
Source Datajson Identifier True
Source Hash d047c2c625ff6d260e66d52ff671de3a455858df
Source Schema Version 1.1

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