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The Ability of NASA's Meteoroid Engineering Model to Replicate in Situ Impact DataMeteoroid environment models must describe the mass, directionality, velocity, and density distributions of meteoroids in order to correctly predict the rate at which meteoroids impact spacecraft. We present an updated version of NASA's Meteoroid Engineering Model (MEM) that better captures the correlation between directionality and velocity and incorporates a bulk density distribution. We compare the resulting model with the rate of large particle impacts seen on the Long Duration Exposure Facility (LDEF) and the Pegasus I and II satellites. The updated model shows closer agreement with these in situ data than previous versions of MEM.
Document ID
20180007868
Acquisition Source
Marshall Space Flight Center
Document Type
Abstract
Authors
Moorhead, Althea V.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
November 27, 2018
Publication Date
October 21, 2018
Subject Category
Space Sciences (General)
Report/Patent Number
M18-6855
Report Number: M18-6855
Meeting Information
Meeting: Division for Planetary Sciences
Location: Knoxville, TN
Country: United States
Start Date: October 21, 2018
End Date: October 26, 2018
Sponsors: American Astronomical Society
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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