BS ISO 23339:2010
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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Space systems. Unmanned spacecraft. Estimating the mass of remaining usable propellant
Hardcopy , PDF
04-08-2022
English
31-07-2011
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Superseded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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