PD ISO/TR 18146:2015
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
Space systems. Space debris mitigation design and operation guidelines for spacecraft
Hardcopy , PDF
28-10-2020
English
31-10-2015
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Foreword
Introduction
1 Scope
2 Related documents and abbreviated terms and symbols
3 Requirements in ISO standards and system-level
methodologies for complying with them.6
4 Debris-related work in the development cycle
5 System-level considerations
6 Subsystem/component design and operation
Defines non-normative information on spacecraft design and operational practices for mitigating space debris.
| Committee |
ACE/68
|
| DocumentType |
Standard
|
| Pages |
64
|
| PublisherName |
British Standards Institution
|
| Status |
Superseded
|
| SupersededBy |
| Standards | Relationship |
| 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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