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ISO/TR 18146:2015

Withdrawn

Withdrawn

A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

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withdrawn

A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.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 Space debris mitigation design and operation guidelines for spacecraft

Available format(s)

Hardcopy , PDF , PDF 3 Users , PDF 5 Users , PDF 9 Users

Withdrawn date

10-11-2020

Language(s)

English

Published date

01-10-2015

ISO/TR 18146:2015 contains non-normative information on spacecraft design and operational practices for mitigating space debris.

ISO/TR 18146:2015 is a supporting document to the family of international standards addressing space debris mitigation (see 2.2). The purpose of these standards is to minimize the creation of additional space debris by ensuring that spacecraft and launch vehicle orbital stages are designed, operated and disposed of in a manner that prevents them from generating debris throughout their orbital lifetime.

ISO/TR 18146:2015 can be used to guide spacecraft engineers in the application of these space debris mitigation standards. Table 1 lists the main debris mitigation requirements defined in the standards and compares them to equivalent recommendations published by the United Nations and the Inter-Agency Space Debris Coordination Committee.

DocumentType
Technical Report
Pages
50
PublisherName
International Organization for Standardization
Status
Withdrawn
SupersededBy

Standards Relationship
PD ISO/TR 18146:2015 Identical

ISO 16404:2013 Space systems Programme management Requirements management
ISO 14200:2012 Space environment (natural and artificial) Guide to process-based implementation of meteoroid and debris environmental models (orbital altitudes below GEO + 2 000 km)
ISO 16126:2014 Space systems — Assessment of survivability of unmanned spacecraft against space debris and meteoroid impacts to ensure successful post-mission disposal
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 27025:2010 Space systems — Programme management — Quality assurance requirements
ISO/TR 11233:2014 Space systems Orbit determination and estimation Process for describing techniques
ISO/TR 11225:2012 Space environment (natural and artificial) — Guide to reference and standard atmosphere models
ISO 14300-1:2011 Space systems — Programme management — Part 1: Structuring of a project
ISO 27852:2016 Space systems — Estimation of orbit lifetime
ISO 26872:2010 Space systems Disposal of satellites operating at geosynchronous altitude
ISO 23339:2010 Space systems — Unmanned spacecraft — Estimating the mass of remaining usable propellant
ISO/TR 16158:2013 Space systems Avoiding collisions with orbiting objects
ISO 14623:2003 Space systems - Pressure vessels and pressurized structures Design and operation
ISO 11227:2012 Space systems — Test procedure to evaluate spacecraft material ejecta upon hypervelocity impact
ISO 16164:2015 Space systems — Disposal of satellites operating in or crossing Low Earth Orbit

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