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BS ISO 23339:2010

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by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. Unmanned spacecraft. Estimating the mass of remaining usable propellant

Available format(s)

Hardcopy , PDF

Superseded date

04-08-2022

Superseded by

BS ISO 23312:2022

Language(s)

English

Published date

31-07-2011

€156.59
Excluding VAT

Foreword
Introduction
1 Scope
2 Normative references
3 Terms and definitions
4 Objectives
5 Requirements
Annex A (informative) - Examples of estimation methods
Bibliography

Provides 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.

Committee
ACE/68
DevelopmentNote
Supersedes 08/30147932 DC. (07/2011)
DocumentType
Standard
Pages
16
PublisherName
British Standards Institution
Status
Superseded
SupersededBy
Supersedes

This International Standard 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.

Standards Relationship
ISO 23339:2010 Identical

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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