ISO 16699:2015
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
Space systems Disposal of orbital launch stages
Hardcopy , PDF , PDF 3 Users , PDF 5 Users , PDF 9 Users
17-12-2021
English
16-11-2015
ISO 16699:2015 focuses on disposal of launch vehicle stages used during launch of spacecraft to be operated in space where the orbital launch stages are left in orbit after the spacecraft are released.
End-of-mission disposal of launch vehicle orbital stages broadly means removing the stages from the protected regions of space (see ISO 24113) so as not to collide or otherwise interfere with the other users of those protected regions in the future. ISO 24113 also requires that "During the disposal phase, a spacecraft or launch vehicle orbital stage shall permanently deplete or make safe all remaining on-board sources of stored energy in a controlled sequence." These "passivation" actions are typically either accomplished in the course of disposal, or immediately follow the disposal operations. In this document, the term "disposal actions" refers to both disposal manoeuvres and to passivation actions (note: passivation actions are not required after the final manoeuvre leading to a controlled re-entry).
ISO 24113 provides six options for spacecraft or orbital launch stage disposal. This International Standard specifies techniques for planning and executing disposal of orbital launch stages that are consistent with ISO 24113 requirements, reflect current internationally accepted guidelines, and consider current operational procedures and best practices.
DevelopmentNote |
Supersedes ISO/DIS 16699. (11/2015)
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DocumentType |
Standard
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Pages |
6
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PublisherName |
International Organization for Standardization
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Status |
Withdrawn
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Standards | Relationship |
BS ISO 16699:2015 | Identical |
14/30213848 DC : 0 | BS ISO 16164 - SPACE SYSTEMS - DISPOSAL OF SATELLITES OPERATING IN OR CROSSING LOW EARTH ORBIT |
ISO/TR 20590:2017 | Space systems - Debris mitigation design and operation manual for launch vehicle orbital stages |
PD ISO/TR 20590:2017 | Space systems. Debris mitigation design and operation manual for launch vehicle orbital stages |
ISO 14303:2002 | Space systems — Launch-vehicle-to-spacecraft interfaces |
ISO 27875:2010 | Space systems Re-entry risk management for unmanned spacecraft and launch vehicle orbital stages |
ISO 16127:2014 | Space systems — Prevention of break-up of unmanned spacecraft |
ISO 24113:2011 | Space systems Space debris mitigation requirements |
ISO 17401:2004 | Space systems — Spacecraft interface requirements document for launch vehicle services |
ISO 15864:2004 | Space systems General test methods for space craft, subsystems and units |
ISO 27852:2016 | Space systems — Estimation of orbit lifetime |
ISO 26872:2010 | Space systems Disposal of satellites operating at geosynchronous altitude |
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