95.99 Withdrawal of Standard Feb 23, 2024
ISO
ISO/TC 20/SC 14 Space systems and operations
International Standard
49.140 Space systems and operations
ISO 27852:2016 describes a process for the estimation of orbit lifetime for spacecraft, launch vehicles, upper stages and associated debris in LEO-crossing orbits.
It also clarifies the following:
a) modelling approaches and resources for solar and geomagnetic activity modelling;
b) resources for atmosphere model selection;
c) approaches for spacecraft ballistic coefficient estimation.
WITHDRAWN
ISO 27852:2011
WITHDRAWN
ISO 27852:2016
95.99
Withdrawal of Standard
Feb 23, 2024
PUBLISHED
ISO 27852:2024