ISO 23339:2010 PDF
Space systems — Unmanned spacecraft — Estimating the mass of remaining usable propellant
Open preview (PDF)Space systems — Unmanned spacecraft — Estimating the mass of remaining usable propellantTitle (English):
ISO 23339:2010
Space systems — Unmanned spacecraft — Estimating the mass of remaining usable propellant
- Document status:
- Withdrawn
- Format:
- Electronic (PDF)
- Number of pages:
- 7
- Publication date:
- November 24, 2010
- Edition:
- ISO IS 23339 edition 1 version 1
- ICS:
- 49.140
Description (English):
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.
Technical details
- Technical committee
- ISO/TC 20/SC 14 - Space systems and operations
- SKU
- ISO 23339:2010
