Baseline micrometeoroid and orbital debris fluence estimates for spacecraft in low Earth orbit (LEO) are provided. For these calculations, an orbit similar to that of the International Space Station (ISS) is used.
Micrometeoroid and Orbital Debris Environments for the International Space Station
2007
12 pages
Report
No indication
English
Astronomy & Celestial Mechanics , Manned Spacecraft , Spacecraft , Earth orbits , Meteoroids , Space stations , Damage , Particles , International , Comets , Asteroids , Silicates , Radiofrequency , Base lines , Estimates , Debris , Orbital debris environments , Micrometeoroids and oribital debris , Leo(Low earth orbit) , Iss(International space station) , Mmod(Micrometeoroids and oribital debris) , Plasma discharges , Sed(Sudden electrical disturbance) , Risk assessment
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