ISO 23339:2010

Retirada (Edición 1, 2010)

Nueva versión disponible: 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

Estado
: Retirada

Fecha de publicación
: 2010-12

Etapa
: Retirada de la Norma Internacional [95.99]
Edición
: 1

Número de páginas
: 7
Comité Técnico :
ISO/TC 20/SC 14

ICS :
49.140
RSS actualizaciones