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ISO 24113:2011

Withdrawn
Withdrawn

A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

View Superseded by
withdrawn

A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.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

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

Withdrawn date

07-12-2019

Language(s)

English

Published date

05-11-2011

Publisher

International Organization for Standardization

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Withdrawn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

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Hardcopy - English
PDF - English
PDF 3 Users - English
PDF 5 Users - English
PDF 9 Users - English
Hardcopy - English
PDF - English
PDF 3 Users - English
PDF 5 Users - English
PDF 9 Users - English
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