ISO 24113:2011
Withdrawn
View Superseded by
Space systems — Space debris mitigation requirements
Hardcopy , PDF
English
05-11-2011
04-09-2025
ISO 24113:2011 defines the primary space debris mitigation requirements applicable to all elements of unmanned systems launched into, or passing through, near-Earth space, including launch vehicle orbital stages, operating spacecraft and any objects released as part of normal operations or disposal actions.
The requirements contained in ISO 24113:2011 are intended to reduce the growth of 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 24113:2011 is the top-level standard in a family of standards addressing debris mitigation. It will be the main interface for the user, bridging between the primary debris mitigation requirements and the lower-level implementation standards that will ensure compliance.
ISO 24113:2011 does not cover launch phase safety for which specific rules are defined elsewhere.
| Committee |
ISO/TC 20/SC 14
|
| DevelopmentNote |
Supersedes ISO/DIS 24113. (05/2011)
|
| DocumentType |
Standard
|
| Pages |
13
|
| PublisherName |
International Organization for Standardization
|
| Status |
Withdrawn
|
| SupersededBy | |
| Supersedes |
| Standards | Relationship |
| BS ISO 24113:2011 | Identical |
| 12/30213833 DC : 0 | BS ISO 16126 - SPACE SYSTEMS - ASSESSMENT OF SURVIVABILITY OF UNMANNED SPACECRAFT AGAINST SPACE DEBRIS AND METEOROID IMPACTS TO ENSURE SUCCESSFUL POST-MISSION DISPOSAL |
| 15/30303532 DC : 0 | BS ISO 17770 - SPACE SYSTEMS - CUBE SATELLITES (CUBESATS) |
| I.S. EN 16603-10:2018 | SPACE ENGINEERING - SYSTEM ENGINEERING GENERAL REQUIREMENTS |
| BS ISO 17770:2017 | Space systems. Cube satellites (CubeSats) |
| BS ISO 16127:2014 | Space systems. Prevention of break-up of unmanned spacecraft |
| BS ISO 19683:2017 | Space systems. Design qualification and acceptance tests of small spacecraft and units |
| ISO 16164:2015 | Space systems — Disposal of satellites operating in or crossing Low Earth Orbit |
| BS ISO 27852:2016 | Space systems. Estimation of orbit lifetime |
| PD ISO/TR 18146:2015 | Space systems. Space debris mitigation design and operation guidelines for spacecraft |
| 11/30237421 DC : 0 | BS ISO 11227 - SPACE SYSTEMS - TEST PROCEDURE TO EVALUATE SPACECRAFT MATERIAL EJECTA UPON HYPERVELOCITY IMPACT |
| ISO 19683:2017 | Space systems — Design qualification and acceptance tests of small spacecraft and units |
| I.S. EN 16601-00-01:2015 | SPACE SYSTEMS - GLOSSARY OF TERMS |
| 10/30197704 DC : 0 | BS ISO 10784-2 - SPACE SYSTEMS - EARLY OPERATIONS - PART 2: INITIALIZATION PLAN |
| BS ISO 16699:2015 | Space systems. Disposal of orbital launch stages |
| BS ISO 16126:2014 | Space systems. Assessment of survivability of unmanned spacecraft against space debris and meteoroid impacts to ensure successful post-mission disposal |
| 14/30213848 DC : 0 | BS ISO 16164 - SPACE SYSTEMS - DISPOSAL OF SATELLITES OPERATING IN OR CROSSING LOW EARTH ORBIT |
| ISO 27852:2016 | Space systems — Estimation of orbit lifetime |
| ISO 11227:2012 | Space systems — Test procedure to evaluate spacecraft material ejecta upon hypervelocity impact |
| ISO 16699:2015 | Space systems — Disposal of orbital launch stages |
| ISO/TR 20590:2017 | Space systems - Debris mitigation design and operation manual for launch vehicle orbital stages |
| BS ISO 11227:2012 | Space systems. Test procedure to evaluate spacecraft material ejecta upon hypervelocity impact |
| BS ISO 23339:2010 | Space systems. Unmanned spacecraft. Estimating the mass of remaining usable propellant |
| 11/30204140 DC : 0 | BS ISO 14200 - SPACE ENVIRONMENT (NATURAL AND ARTIFICIAL) - GUIDE TO PROCESS-BASED IMPLEMENTATION OF METEOROID AND DEBRIS ENVIRONMENTAL MODELS (ORBITAL ALTITUDES BELOW GEO + 2000 KM) |
| ISO 23339:2010 | Space systems — Unmanned spacecraft — Estimating the mass of remaining usable propellant |
| BS ISO 26872:2010 | Space systems. Disposal of satellites operating at geosynchronous altitude |
| EN 16603-10:2018 | Space engineering - System engineering general requirements |
| 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) |
| 12/30213836 DC : 0 | BS ISO 16127 - SPACE SYSTEMS - PREVENTION OF BREAK-UP OF UNMANNED SPACECRAFT |
| BS EN 16601-00-01:2015 | Space systems. Glossary of terms |
| 13/30235933 DC : 0 | BS ISO 16699 - SPACE SYSTEMS - DISPOSAL OF ORBITAL LAUNCH STAGES |
| BS ISO 16164:2015 | Space systems. Disposal of satellites operating in or crossing Low Earth Orbit |
| BS 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) |
| BS ISO 10784-1:2011 | Space systems. Early operations Spacecraft initialization and commissioning |
| ISO 26872:2010 | Space systems — Disposal of satellites operating at geosynchronous altitude |
| 15/30324485 DC : 0 | BS ISO 27852 - SPACE SYSTEMS - ESTIMATION OF ORBIT LIFETIME |
| BS ISO 27875 : 2010 | SPACE SYSTEMS - RE-ENTRY RISK MANAGEMENT FOR UNMANNED SPACECRAFT AND LAUNCH VEHICLE ORBITAL STAGES |
| ISO 27875:2010 | Space systems — Re-entry risk management for unmanned spacecraft and launch vehicle orbital stages |
| ISO 16126:2014 | Space systems — Assessment of survivability of unmanned spacecraft against space debris and meteoroid impacts to ensure successful post-mission disposal |
| ISO/TR 18146:2015 | Space systems — Space debris mitigation design and operation guidelines for spacecraft |
| BS ISO 17546:2016 | Space systems. Lithium ion battery for space vehicles. Design and verification requirements |
| EN 16601-00-01:2015 | Space systems - Glossary of terms |
| 10/30197700 DC : 0 | BS ISO 10784-1 - SPACE SYSTEMS - EARLY OPERATIONS - PART 1: SPACECRAFT INITIALIZATION AND COMMISSIONING |
| 16/30302535 DC : 0 | BS ISO 19683 - SPACE SYSTEMS - DESIGN QUALIFICATION AND ACCEPTANCE TESTS OF SMALL SPACECRAFT AND UNITS |
| PD ISO/TR 20590:2017 | Space systems. Debris mitigation design and operation manual for launch vehicle orbital stages |
| ISO 16127:2014 | Space systems — Prevention of break-up of unmanned spacecraft |
| ISO 17770:2017 | Space systems — Cube satellites (CubeSats) |
| ISO 10784-1:2011 | Space systems — Early operations — Part 1: Spacecraft initialization and commissioning |
| ISO 17546:2016 | Space systems — Lithium ion battery for space vehicles — Design and verification requirements |
| ISO 9000:2015 | Quality management systems — Fundamentals and vocabulary |
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