SS-ISO-15859-7 › Space systems - Fluid characteristics, sampling and test methods - Part 7: Hydrazine propellant (ISO 15859-7:2004, IDT)
SS-ISO-15859-7
-
2004 EDITION
-
CURRENT
Document Center Inc. is an authorized dealer of SIS standards.
The following bibliographic material is provided to assist you with your purchasing decision:
The following bibliographic material is provided to assist you with your purchasing decision:
This part of ISO 15859 specifies limits for the composition and physical properties of anhydrous hydrazine (N2H4) and establishes the sampling and test requirements applicable for the verification of the anhydrous hydrazine composition. This part of ISO 15859 is applicable to anhydrous hydrazine propellant, intended for use as fuel in propellant systems of space systems as well as in both flight hardware and ground facilities, systems, and equipment, of the following grades. -- Standard: normal production and quality control (suitable for most uses). -- Monopropellant: normal product with strict control of specified impurities (to be specified only for monopropellant catalytic engines where extended life of the catalyst is desired). -- High purity: special production with strict control of specified impurities. This part of ISO 15859 is applicable to influents only within the specified limits herein. Hydrazine may be of the liquid type. This part of ISO 15859 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 to for a particular use.
To find similar documents by classification:
This document comes with our free Notification Service, good for the life of the document.
This document is available in either Paper or PDF format.
Designation Name
SS-ISO 15859-7:2004
Revision Level
2004 EDITION
Status
Current
Publication Date
Aug. 6, 2004
Language(s)
English
Page Count
10
International Equivalent
ISO 15849-7:2004(IDT)