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     : Withdrawn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
  • Edition
     : 1
    Number of pages
     : 7
  • Technical Committee
     : ISO/TC 20/SC 14 Space systems and operations
  • ICS
     :
    49.140 Space systems and operations

Life cycle

Sustainable Development Goals

This standard contributes to the following Sustainable Development Goal

9
Industry, Innovation and Infrastructure

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