ISO-27875 › Historical Revision Information
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

ISO-27875 - FOR 2ND EDITION AMENDMENT 1 SEE - CURRENT -- See the following: ISO-27875-AM1
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ISO 27875:2010 provides a framework with which to assess, reduce and control the potential risks that spacecraft and launch vehicle orbital stages pose to people and the environment when those space vehicles re-enter the Earth's atmosphere and impact the Earth's surface. It is intended to be applied to the planning, design and review of space vehicle missions for which controlled or uncontrolled re-entry is possible.

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49.140 (Space systems and operations Including space data and information transfer systems, and ground support equipment for launch site operations)

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Document Number

ISO-27875

Revision Level

FOR 2ND EDITION AMENDMENT 1 SEE

Status

Current

Publication Date

Sept. 1, 2020

Committee Number

ISO/TC 20/SC 14