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Final Results of Shuttle MMOD Impact DatabaseThe Shuttle Hypervelocity Impact Database documents damage features on each Orbiter thought to be from micrometeoroids (MM) or orbital debris (OD). Data is divided into tables for crew module windows, payload bay door radiators and thermal protection systems along with other miscellaneous regions. The combined number of records in the database is nearly 3000. Each database record provides impact feature dimensions, location on the vehicle and relevant mission information. Additional detail on the type and size of particle that produced the damage site is provided when sampling data and definitive spectroscopic analysis results are available. Guidelines are described which were used in determining whether impact damage is from micrometeoroid or orbital debris impact based on the findings from scanning electron microscopy chemical analysis. Relationships assumed when converting from observed feature sizes in different shuttle materials to particle sizes will be presented. A small number of significant impacts on the windows, radiators and wing leading edge will be highlighted and discussed in detail, including the hypervelocity impact testing performed to estimate particle sizes that produced the damage.
Document ID
20140009919
Acquisition Source
Johnson Space Center
Document Type
Abstract
Authors
Hyde, J. L.
(Barrios Technology, Inc. Houston, TX, United States)
Christiansen, E. L.
(NASA Johnson Space Center Houston, TX, United States)
Lear, D. M.
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
July 21, 2014
Publication Date
April 26, 2015
Subject Category
Space Transportation And Safety
Report/Patent Number
JSC-CN-31407
Report Number: JSC-CN-31407
Meeting Information
Meeting: Hypervelocity Impact Symposium
Location: Boulder, CO
Country: United States
Start Date: April 26, 2015
End Date: April 30, 2015
Sponsors: Hypervelocity Impact Society
Distribution Limits
Public
Copyright
Public Use Permitted.
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