Homepage>ISO Standards>ISO 27875:2019/Amd 1:2020-Space systems — Re-entry risk management for unmanned spacecraft and launch vehicle orbital stages-Amendment 1: Formula to obtain Ec by the product of the probability of impact on a specific latitude band, and the population within the band, which is integrated over the latitude range covered by the orbital inclination
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ISO 27875:2019/Amd 1:2020
ISO 27875:2019/Amd 1:2020-Space systems — Re-entry risk management for unmanned spacecraft and launch vehicle orbital stages-Amendment 1: Formula to obtain Ec by the product of the probability of impact on a specific latitude band, and the population within the band, which is integrated over the latitude range covered by the orbital inclination
