Buy this standard

Abstract Preview

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 :  Published
    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

Sustainable Development Goals

This standard contributes to the following Sustainable Development Goal:

9
Industry, Innovation and Infrastructure

Buy this standard

Format Language
PDF
Paper
  • CHF58

Life cycle


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)

Keep up to date with ISO

Sign up to our newsletter for the latest news, views and product information.

  2. Store
  3. Standards catalogue
  4. TC
  5. ISO/TC 20/SC 14
  6. ISO 23339:2010