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A Method to have Multi-Layer Thermal Insulation Provide Damage DetectionDesign and testing of a multi-layer thermal insulation system that also provides debris and micrometeorite damage detection is presented. One layer of the insulation is designed as an array of passive open-circuit electrically conductive spiral trace sensors. The sensors are a new class of sensors that are electrically open-circuits that have no electrical connections thereby eliminating one cause of failure to circuits. The sensors are powered using external oscillating magnetic fields. Once electrically active, they produce their own harmonic magnetic fields. The responding field frequency changes if any sensor is damaged. When the sensors are used together in close proximity, the inductive coupling between sensors provides a means of telemetry. The spiral trace design using reflective electrically conductive material provides sufficient area coverage for the sensor array to serves as a layer of thermal insulation. The other insulation layers are designed to allow the sensor s magnetic field to permeate the insulation layers while having total reflective surface area to reduce thermal energy transfer. Results of characterizing individual sensors and the sensor array s response to punctures are presented. Results of hypervelocity impact testing using projectiles of 1-3.6 millimeter diameter having speeds ranging from 6.7-7.1 kilometers per second are also presented.
Document ID
20070018342
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Woodward, Stanley E.
(NASA Langley Research Center Hampton, VA, United States)
Taylor, Bryant D.
(Swales Aerospace Hampton, VA, United States)
Jones, Thomas W.
(NASA Langley Research Center Hampton, VA, United States)
Shams, Qamar A.
(NASA Langley Research Center Hampton, VA, United States)
Lyons, Frankel
(Hamilton Sundstrand Corp. Houston, TX, United States)
Henderson, Donald
(NASA White Sands Test Facility NM, United States)
Date Acquired
August 23, 2013
Publication Date
January 1, 2007
Subject Category
Lunar And Planetary Science And Exploration
Report/Patent Number
AIAA 2007-1847
LAR-17294
LAR-17295
Report Number: AIAA 2007-1847
Report Number: LAR-17294
Report Number: LAR-17295
Meeting Information
Meeting: 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
Location: Waikiki, HI
Country: United States
Start Date: April 23, 2007
End Date: April 26, 2007
Sponsors: American Society of Mechanical Engineers, American Inst. of Aeronautics and Astronautics, American Society of Civil Engineers, American Helicopter Society, Inc.
Distribution Limits
Public
Copyright
Public Use Permitted.
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