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ISO 27852:2016

Withdrawn

Withdrawn

View Superseded by

Space systems — Estimation of orbit lifetime

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

07-04-2016

Withdrawn date

04-09-2025

Superseded by

ISO 27852:2024

US$96.00
Excluding Tax where applicable

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.

Committee
ISO/TC 20/SC 14
DevelopmentNote
Supersedes ISO/DIS 27852. (07/2016)
DocumentType
Standard
Pages
43
PublisherName
International Organization for Standardization
Status
Withdrawn
SupersededBy
Supersedes
UnderRevision

Standards Relationship
BS ISO 27852:2016 Identical

ISO 16164:2015 Space systems — Disposal of satellites operating in or crossing Low Earth Orbit
BS ISO 16699:2015 Space systems. Disposal of orbital launch stages
ISO/TR 20590:2017 Space systems - Debris mitigation design and operation manual for launch vehicle orbital stages
14/30213848 DC : 0 BS ISO 16164 - SPACE SYSTEMS - DISPOSAL OF SATELLITES OPERATING IN OR CROSSING LOW EARTH ORBIT
ISO 16699:2015 Space systems — Disposal of orbital launch stages
13/30235933 DC : 0 BS ISO 16699 - SPACE SYSTEMS - DISPOSAL OF ORBITAL LAUNCH STAGES
BS ISO 16164:2015 Space systems. Disposal of satellites operating in or crossing Low Earth Orbit
PD ISO/TR 18146:2015 Space systems. Space debris mitigation design and operation guidelines for spacecraft
ISO/TR 18146:2015 Space systems — Space debris mitigation design and operation guidelines for spacecraft
PD ISO/TR 20590:2017 Space systems. Debris mitigation design and operation manual for launch vehicle orbital stages

ISO 24113:2011 Space systems — Space debris mitigation requirements

US$96.00
Excluding Tax where applicable