Orbital Debris Risk Assessment System
Liu You-ying
Abstract
Liu You-ying
Abstract
A GUI based meteoroid and orbital debris risk assessment system(MODRAS) is developed for assessing risks to spacecraft from meteoroid and debris impact.Instance a spacecraft as an example for M/OD risk assessment is conducted.The distribution of debris flux,exposed area of spacecraft and impact data are obtained.The results show that the relative impact possibility for a spacecraft depends on the spacecraft's altitude and orbital inclination,as well as debris size.Changes in shuttle mission operations,flight rules,and flight planning were adopted to reduce meteoroid and debris risks.
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A GUI based meteoroid and orbital debris risk assessment system(MODRAS) is developed for assessing risks to spacecraft from meteoroid and debris impact.Instance a spacecraft as an example for M/OD risk assessment is conducted.The distribution of debris flux,exposed area of spacecraft and impact data are obtained.The results show that the relative impact possibility for a spacecraft depends on the spacecraft's altitude and orbital inclination,as well as debris size.Changes in shuttle mission operations,flight rules,and flight planning were adopted to reduce meteoroid and debris risks.
Key concepts: Spacecraft, Meteoroid, Space debris, Debris, Aerospace engineering, Environmental science, Orbital inclination, Flight planning