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ISO 23339:2010

Space systems — Unmanned spacecraft — Estimating the mass of remaining usable propellant
24 nën 2010
95.99 Withdrawal of Standard   14 korr 2022

General information

95.99     14 korr 2022

ISO

ISO/TC 20/SC 14

International Standard

49.140  

anglisht  

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Scope

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.

Life cycle

NOW

WITHDRAWN
ISO 23339:2010
95.99 Withdrawal of Standard
14 korr 2022

REVISED BY

PUBLISHED
ISO 23312:2022