ISO 23339:2010 PDF
Space systems — Unmanned spacecraft — Estimating the mass of remaining usable propellant
Название (английский):
ISO 23339:2010
Space systems — Unmanned spacecraft — Estimating the mass of remaining usable propellant
- Статус документа:
- Отменён
- Формат:
- Электронный (PDF)
- Количество страниц:
- 7
- Дата публикации:
- 24 ноября 2010 г.
- Издание:
- ISO IS 23339 edition 1 version 1
- ICS:
- 49.140
Описание (английский):
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.
Технические детали
- Технический комитет
- ISO/TC 20/SC 14 - Space systems and operations
- SKU
- ISO 23339:2010