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Space station integrated wall damage and penetration damage control. Task 5: Space debris measurement, mapping and characterization systemThe procedures and results of a study of a conceptual system for measuring the debris environment on the space station is discussed. The study was conducted in two phases: the first consisted of experiments aimed at evaluating location of impact through panel response data collected from acoustic emission sensors; the second analyzed the available statistical description of the environment to determine the probability of the measurement system producing useful data, and analyzed the results of the previous tests to evaluate the accuracy of location and the feasibility of extracting impactor characteristics from the panel response. The conclusions were that for one panel the system would not be exposed to any event, but that the entire Logistics Module would provide a modest amount of data. The use of sensors with higher sensitivity than those used in the tests could be advantageous. The impact location could be found with sufficient accuracy from panel response data. The waveforms of the response were shown to contain information on the impact characteristics, but the data set did not span a sufficient range of the variables necessary to evaluate the feasibility of extracting the information.
Document ID
19880008304
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Lempriere, B. M.
(Boeing Aerospace Co. Seattle, WA, United States)
Date Acquired
September 5, 2013
Publication Date
December 16, 1987
Subject Category
Astronautics (General)
Report/Patent Number
D180-30708-1
NAS 1.26:179281
NASA-CR-179281
Report Number: D180-30708-1
Report Number: NAS 1.26:179281
Report Number: NASA-CR-179281
Accession Number
88N17688
Funding Number(s)
CONTRACT_GRANT: NAS8-36426
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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