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ISO 23339:2010

Space systems — Unmanned spacecraft — Estimating the mass of remaining usable propellant
24. 11. 2010.
95.99   Povučen   14. 7. 2022.

Опште информације

95.99     14. 7. 2022.

ISO

ISO/TC 20/SC 14

Međunarodni standard

49.140  

engleski  

Kupovina

Povučen

Jezik na kome želite da primite dokument.

Apstrakt

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.

Životni ciklus

TRENUTNO

POVUČEN
ISO 23339:2010
95.99 Povučen
14. 7. 2022.

REVIDIRAN OD

OBJAVLJEN
ISO 23312:2022