ISO 14951-7:1999
Space systems - Fluid characteristics - Part 7: Hydrazine propellant
- Standard No.
- ISO 14951-7:1999
- Release Date
- 1999
- Published By
- International Organization for Standardization (ISO)
- Status
- Replace By
- ISO 14951-7:1999/Cor 1:2004
- Latest
- ISO 14951-7:1999/Cor 1:2004
- Scope
- This part of ISO 14951 specifies limits for the chemical composition and physical properties of hydrazine (N2H4) propellant and test methods for verification of propellant composition. This part of ISO 14951 is applicable to hydrazine propellant of the following grades, intended for use as a fuel in propellant systems of space systems: — 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 14951 is applicable to propellant used in both flight hardware and ground facilities, systems, and equipment. It is applicable to influents only to the extent specified herein. CAUTION — Hydrazine, in the liquid or vapour form, is toxic and volatile. Care should be taken in the handling and storage of hydrazine to prevent contact with the human body and with materials that are not compatible.
ISO 14951-7:1999 history
- 2004 ISO 14951-7:1999/Cor 1:2004 Space systems - Fluid characteristics - Part 7: Hydrazine propellant; Technical Corrigendum 1
- 1999 ISO 14951-7:1999 Space systems - Fluid characteristics - Part 7: Hydrazine propellant
