The ratio of hazardous meteoroids to orbital debris in near-Earth space |
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Authors: | Althea V. Moorhead Mark Matney |
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Affiliation: | 1. NASA Meteoroid Environment Office, Marshall Space Flight Center, Huntsville, AL 35812, USA;2. NASA Orbital Debris Program Office, Johnson Space Center, Houston, TX 77058, USA |
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Abstract: | Orbital debris is known to pose a substantial threat to Earth-orbiting spacecraft at certain altitudes. For instance, the orbital debris flux near Sun-synchronous altitudes of 600–800 km is particularly high due in part to the 2007 Fengyun-1C anti-satellite test and the 2009 Iridium-Kosmos collision. At other altitudes, however, the orbital debris population is minimal and the primary impactor population is not man-made debris particles but naturally occurring meteoroids. While the spacecraft community has some awareness of the risk posed by debris, there is a common misconception that orbital debris impacts dominate the risk at all locations. In this paper, we present a damage-limited comparison between meteoroids and orbital debris near the Earth for a range of orbital altitude and inclination, using NASA’s latest models for each environment. Overall, orbital debris dominates the impact risk between altitudes of 600 and 1300 km, while meteoroids dominate below 270 km and above 4800 km. |
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Keywords: | Meteoroids Orbital debris Space environments Risk assessment |
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