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.
This International Standard also clarifies the following:
modelling approaches and resources for solar and geomagnetic activity modelling;
resources for atmosphere model selection;
approaches for spacecraft ballistic coefficient estimation.
Document identifier
ISO 27852:2016
Title
Space systems - Estimation of orbit lifetime
ISO Category
TC 20/SC 14: Space systems and operations
Publication date
2016-07-01
International Relationship
BS ISO 27852:2016
History of version
ISO 27852:2016 * ISO 27852:2011
Price |
185 vnd |