ISO 27875:2019/Amd 1:2020
For ISO 27875:2019/Amd 1:2020, item title is 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over the latitude range covered by the orbital inclination; status code is 9599; successor is ISO 27875:2026; withdrawn / published date is 2020-09-08, recorded from its source on 2026-08-05.
- Identifier
- ISO 27875:2019/Amd 1:2020 verified
- Item title
- 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 verified
- Status code
- 9599
- Successor
- ISO 27875:2026
- Withdrawn / published date
- 2020-09-08
Verified
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What the source says
80027,IS,Amd,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","Systèmes spatiaux — Gestion du risque de la rentrée pour les étapes orbitales des véhicules spatiaux non habités et des lanceurs spatiaux — Amendement 1: Formule pour calculer les pertes humaines attendues (Ec) via le produit de la probabilité d'impact sur une bande de latitude spécifique et de la population de cette bande, qui est i
— isopublicstorageprod.blob.core.windows.net, retrieved 2026-08-05
Source
- isopublicstorageprod.blob.core.windows.nethttps://isopublicstorageprod.blob.core.windows.net/opendata/_latest/iso_deliverables_metadata/csv/iso_deliverables_metadata.csv