ISO 23339:2010
w
ISO 23339:2010
55368

Estado : Retirada

Esta norma ha sido revisada por ISO 23312:2022

Resumen

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.

Informaciones generales

  •  : Retirada
     : 2010-12
    : Retirada de la Norma Internacional [95.99]
  •  : 1
     : 7
  • ISO/TC 20/SC 14
    49.140 
  • RSS actualizaciones

Got a question?

Check out our FAQs

Customer care
+41 22 749 08 88

Opening hours:
Monday to Friday - 09:00-12:00, 14:00-17:00 (UTC+1)