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MMOD Protection and Degradation Effects for Thermal Control SystemsMicrometeoroid and orbital debris (MMOD) environment overview Hypervelocity impact effects & MMOD shielding MMOD risk assessment process Requirements & protection techniques - ISS - Shuttle - Orion/Commercial Crew Vehicles MMOD effects on spacecraft systems & improving MMOD protection - Radiators Coatings - Thermal protection system (TPS) for atmospheric entry vehicles Coatings - Windows - Solar arrays - Solar array masts - EVA Handrails - Thermal Blankets Orbital Debris provided by JSC & is the predominate threat in low Earth orbit - ORDEM 3.0 is latest model (released December 2013) - http://orbitaldebris.jsc.nasa.gov/ - Man-made objects in orbit about Earth impacting up to 16 km/s average 9-10 km/s for ISS orbit - High-density debris (steel) is major issue Meteoroid model provided by MSFC - MEM-R2 is latest release - http://www.nasa.gov/offices/meo/home/index.html - Natural particles in orbit about sun Mg-silicates, Ni-Fe, others - Meteoroid environment (MEM): 11-72 km/s Average 22-23 km/s.
Document ID
20140010668
Acquisition Source
Johnson Space Center
Document Type
Presentation
Authors
Christiansen, Eric
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 15, 2014
Publication Date
August 4, 2014
Subject Category
Fluid Mechanics And Thermodynamics
Space Transportation And Safety
Report/Patent Number
JSC-CN-31798
Meeting Information
Meeting: Thermal and Fluids Analysis Workshop 2014 (TFAWS)
Location: Cleveland, OH
Country: United States
Start Date: August 4, 2014
End Date: August 8, 2014
Sponsors: NASA Glenn Research Center
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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