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BS ISO 27852:2016

Superseded

Superseded

View Superseded by

Space systems. Estimation of orbit lifetime

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

07-31-2016

Superseded date

02-29-2024

Superseded by

BS ISO 27852:2024

US$473.61
Excluding Tax where applicable

Foreword
Introduction
1 Scope
2 Normative References
3 Terms, definitions, symbols and abbreviated terms
4 Orbit lifetime estimation
5 Orbit lifetime estimation methods and applicability
6 Drag modelling
7 Estimating ballistic coefficient (C[D]A/m)
Annex A (informative) - Space population distribution
Annex B (informative) - 25-year lifetime predictions using
        random draw approach
Annex C (informative) - Solar radiation pressure and 3rd-body
        perturbations
Annex D (informative) - Sample code for drag coefficient
        estimation via panel model
Bibliography

Specifies a process for the estimation of orbit lifetime for spacecraft, launch vehicles, upper stages and associated debris in LEO-crossing orbits.

Committee
ACE/68
DevelopmentNote
Supersedes 15/30324485 DC. (07/2016)
DocumentType
Standard
Pages
54
PublisherName
British Standards Institution
Status
Superseded
SupersededBy
Supersedes

Standards Relationship
ISO 27852:2016 Identical

ISO 24113:2011 Space systems — Space debris mitigation requirements

US$473.61
Excluding Tax where applicable