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ISO 23339:2010

Withdrawn

Withdrawn

A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

View Superseded by

Space systems — Unmanned spacecraft — Estimating the mass of remaining usable propellant

Available format(s)

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

Withdrawn date

14-07-2022

Superseded by

ISO 23312:2022

Language(s)

English

Published date

24-11-2010

£58.00
Excluding VAT

ISO 23339:2010 gives requirements for estimating the mass of the remaining usable propellant of an unmanned spacecraft in low Earth orbit (LEO) or geostationary Earth orbit (GEO), and for designing propellant measurement systems. It is applicable to spacecraft with either mono- or bi-propellant propulsion systems using liquid or gaseous chemical propellants, and is limited to such systems because they are the most common for spacecraft in LEOs and GEOs.

DevelopmentNote
Supersedes ISO/DIS 23339. (11/2010)
DocumentType
Standard
Pages
7
PublisherName
International Organization for Standardization
Status
Withdrawn
SupersededBy

Standards Relationship
BS ISO 23339:2010 Identical

ISO 16164:2015 Space systems — Disposal of satellites operating in or crossing Low Earth Orbit
14/30213848 DC : 0 BS ISO 16164 - SPACE SYSTEMS - DISPOSAL OF SATELLITES OPERATING IN OR CROSSING LOW EARTH ORBIT
BS ISO 16164:2015 Space systems. Disposal of satellites operating in or crossing Low Earth Orbit
PD ISO/TR 18146:2015 Space systems. Space debris mitigation design and operation guidelines for spacecraft
ISO/TR 18146:2015 Space systems Space debris mitigation design and operation guidelines for spacecraft

ISO 24113:2011 Space systems Space debris mitigation requirements
ISO 26872:2010 Space systems Disposal of satellites operating at geosynchronous altitude

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