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Fiber-Optic Micrometeoroid/Orbital Debris Impact Detector SystemA document describes a reliable, lightweight micrometeoroid/orbital debris (MMOD) detection system that can be located at strategic positions of "high consequence" to provide real-time warning of a penetration, its location, and the extent of the damage to a spacecraft. The concept is to employ fiber-optic sensors to detect impact damage and penetration of spacecraft structures. The fibers are non-electrical, employ light waves, and are immune to electromagnetic interference. The fiber-optic sensor array can be made as a stand-alone product, being bonded to a flexible membrane material or a structure that is employed as a MMOD shield material. The optical sensors can also be woven into hybrid MMOD shielding fabrics. The glass fibers of the fiber-optic sensor provide a dual purpose in contributing to the breakup of MMOD projectiles. The grid arrays can be made in a modular configuration to provide coverage over any area desired. Each module can be connected to a central scanner instrument and be interrogated in a continuous or periodic mode.
Document ID
20120010466
Acquisition Source
Johnson Space Center
Document Type
Other - NASA Tech Brief
Authors
Christiansen, Eric L.
(NASA Johnson Space Center Houston, TX, United States)
Tennyson, R. C.
(Fiber Optic Systems Technology System, Inc. Ontario, Canada)
Morison, W. D.
(Fiber Optic Systems Technology System, Inc. Ontario, Canada)
Date Acquired
August 26, 2013
Publication Date
June 1, 2012
Publication Information
Publication: NASA Tech Briefs, June 2012
Subject Category
Man/System Technology And Life Support
Report/Patent Number
MSC-23934-1
Distribution Limits
Public
Copyright
Public Use Permitted.
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