ISO-23339 › Space systems - Unmanned spacecraft - Estimating the mass of remaining usable propellant

ISO-23339 - 1ST EDITION - SUPERSEDED
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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.

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Document Number

ISO 23339:2010

Revision Level

1ST EDITION

Status

Superseded

Publication Date

Dec. 1, 2010

Committee Number

ISO/TC 20/SC 14