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Magnetospheric Multiscale Mission Micrometeoroid/Orbital Debris ImpactsThe MMS spacecraft are highly instrumented (accelerometers, star cameras, Sun sensors, science experiments for plasmas etc.). This presentation will discuss how data from these systems has allowed two micrometeoroid/orbital debris events to be studied: the Feb. 2, 2016 impact with an MMS4 shunt resistor, and the June 12, 2016 impact with an MMS4 wire boom.
Document ID
20170012149
Acquisition Source
Goddard Space Flight Center
Document Type
Presentation
Authors
Williams, Trevor (NASA Goddard Space Flight Center Greenbelt, MD, United States)
Sedlak, Joseph (AI Solutions, Inc. Lanham, MD, United States)
Shulman, Seth (KBRwyle Greenbelt, MD, United States)
Date Acquired
December 14, 2017
Publication Date
December 12, 2017
Subject Category
Astronautics (General)
Spacecraft Instrumentation And Astrionics
Report/Patent Number
GSFC-E-DAA-TN50356
Meeting Information
Meeting: Spacecraft Anomalies and Failure Workshop 2017
Location: Chantilly, VA
Country: United States
Start Date: December 12, 2017
Sponsors: National Reconnaissance Office
Funding Number(s)
CONTRACT_GRANT: NNG17HP02C
CONTRACT_GRANT: NNG14VC09C
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Attitude dynamic
Micrometeoroid/orbital debris

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