ISO 24113:2011
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
View Superseded by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 requirements
Hardcopy , PDF , PDF 3 Users , PDF 5 Users , PDF 9 Users
12-07-2019
English
11-05-2011
Important note : Users cannot be edited or removed once added to your Multi user PDF.
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.
| 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Withdrawn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 |
Access your standards online with a subscription
Features
-
Simple online access to standards, technical information and regulations.
-
Critical updates of standards and customisable alerts and notifications.
-
Multi-user online standards collection: secure, flexible and cost effective.