ISO/TR 18146:2015
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
View Superseded by
Space systems Space debris mitigation design and operation guidelines for spacecraft
Hardcopy , PDF , PDF 3 Users , PDF 5 Users , PDF 9 Users
10-11-2020
English
01-10-2015
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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Withdrawn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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