Reference number
ISO 23339:2010
© ISO 2025
ISO 23339:2010
Space systems — Unmanned spacecraft — Estimating the mass of remaining usable propellant
Edition 1
2010-12
Withdrawn
Withdrawn (Edition 1, 2010)

Abstract

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.

General information

  • Status
     : Withdrawn
    Publication date
     : 2010-12
    Stage
    : Withdrawal of International Standard [95.99]
  • Edition
     : 1
    Number of pages
     : 7
  • Technical Committee :
    ISO/TC 20/SC 14
    ICS :
    49.140 
  • RSS updates

Life cycle

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9
Industry, Innovation and Infrastructure

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