ISO 15859:2004
ISO 15859:2004 Space systems – Fluid characteristics, sampling and test methods – Part 1: Oxygen
CDN $129.00
Description
ISO 15859-1:2004 specifies the limit values for the composition of oxygen and establishes the sampling and test requirements applicable for the verification of the oxygen composition.
ISO 15859-1:2004 is applicable to oxygen used in both flight hardware and ground facilities, systems and equipment, of the following types and grades: Type I, gaseous (Grade A: standard, purging/pressurization, Grade CB: crew breathing, Grade F: fuel-cell) and Type II, liquid (Grade A: oxidize, Grade B: oxidizer, Grade F: fuel-cell).
ISO 15859-1:2004 is applicable to influents only to the extent specified herein.
ISO 15859-1:2004 is applicable to any sampling operation required to ensure that, when the fluid enters the launch vehicle or spacecraft, the fluid composition complies with the limits provided hereafter or with any technical specification agreed for a particular use.
Edition
1
Published Date
2004-06-08
Status
PUBLISHED
Pages
9
Language
English
Format
Secure PDF
Secure – PDF details
- Save your file locally or view it via a web viewer
- Viewing permissions are restricted exclusively to the purchaser
- Device limits - 3
- Printing – Enabled only to print (1) copy
See more about our Environmental Commitment
Abstract
ISO 15859-1:2004 specifies the limit values for the composition of oxygen and establishes the sampling and test requirements applicable for the verification of the oxygen composition.
ISO 15859-1:2004 is applicable to oxygen used in both flight hardware and ground facilities, systems and equipment, of the following types and grades: Type I, gaseous (Grade A: standard, purging/pressurization, Grade CB: crew breathing, Grade F: fuel-cell) and Type II, liquid (Grade A: oxidize, Grade B: oxidizer, Grade F: fuel-cell).
ISO 15859-1:2004 is applicable to influents only to the extent specified herein.
ISO 15859-1:2004 is applicable to any sampling operation required to ensure that, when the fluid enters the launch vehicle or spacecraft, the fluid composition complies with the limits provided hereafter or with any technical specification agreed for a particular use.
Previous Editions
Can’t find what you are looking for?
Please contact us at:
Related Documents
-
ISO 2382:2015 Information technology – Vocabulary
CDN $0.00 Add to cart -
ISO 22553:2019 Paints and varnishes – Electro-deposition coatings – Part 1: Vocabulary
CDN $85.00 Add to cart -
ISO 16520:2025 Tourism and related services – Restaurants and catering – Vocabulary
CDN $192.00 Add to cart -
ISO 80000:2019 Quantities and units – Part 11: Characteristic numbers
CDN $347.00 Add to cart
