ISO 23339:2010
Withdrawn
View Superseded by
Space systems — Unmanned spacecraft — Estimating the mass of remaining usable propellant
Hardcopy , PDF
English
11-24-2010
04-09-2025
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.
| Committee |
ISO/TC 20/SC 14
|
| 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Withdrawn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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