ISO 15859-11:2004
Space systems — Fluid characteristics, sampling and test methods — Part 11: Ammonia
Space systems — Fluid characteristics, sampling and test methods — Part 11: Ammonia
- Статус документа:
- Действующий
- Формат:
- Электронный (PDF)
- Количество страниц:
- 5
- Дата публикации:
- 9 июня 2004 г.
- Издание:
- ISO IS 15859 edition 1 version 1
- ICS:
- 49.140
ISO 15859-11:2004 specifies limits for the composition of ammonia (NH3) and establishes the sampling and test requirements applicable for the verification of the ammonia composition. ISO 15859-11:2004 is applicable to sampling and test methods for ammonia used in both flight hardware and ground support facilities, systems, and equipment. ISO 15859-11:2004 is applicable to ammonia influents only within the specified limits herein. ISO 15859-11:2004 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 to for a particular use.
Abstract
Overview - ISO 15859-11:2004 (Ammonia for space systems)
ISO 15859-11:2004 is the International Standard that defines composition limits, sampling and test methods for ammonia (NH3) used in space systems. It applies to ammonia delivered to launch vehicles, spacecraft and associated ground support facilities and equipment. The standard ensures that ammonia influents meet purity requirements before entering the flight vehicle or spacecraft interface.
Key topics and requirements
- Composition limits:
- Ammonia purity (mass fraction): ≥ 99.99% (determined by indirect method).
- Water content: ≤ 50 µg/g.
- Oil content: ≤ 6 µg/g.
- Chlorides: ≤ 1 µg/g.
- Total non‑volatile residue and fluorides: recorded and reported (informational).
- Test methods:
- Sampling requirements:
- Sampling plan must specify points, procedures, frequency, sample size and responsibilities.
- Supplier responsibility: unless otherwise agreed, the supplier samples and verifies ammonia at the flight vehicle interface.
- Sampling frequency: generally annually or as agreed between supplier and customer.
- Procedures for gaseous and vaporized liquid samples are described; safety and compatibility warnings are emphasized (ammonia is toxic and corrosive to incompatible materials).
- Procurement and rejection: Procure in accordance with national standards where applicable; nonconforming samples must be rejected and disposal handled per customer instructions.
Practical applications and users
- Who uses ISO 15859-11:
- Spacecraft and launch vehicle integrators, launch service providers and ground support engineers.
- Suppliers and transporters of liquefied anhydrous ammonia for space applications.
- Test laboratories, quality assurance teams and safety officers responsible for fluid cleanliness and compatibility.
- Why it matters: Ensures fluid purity, compatibility with flight hardware, and consistent verification procedures across supplier/customer interfaces - reducing contamination risk to propulsion, thermal control or life‑support systems that use ammonia.
Related standards
- ISO 15859 series (Parts 1–13) - fluid characteristics for other spacecraft fluids.
- ISO 7103, ISO 7104, ISO 7105, ISO 7106 - specific sampling and test methods referenced.
- ISO 9000 - quality management terminology and fundamentals.
Keywords: ISO 15859-11, ammonia sampling, ammonia test methods, space systems fluid standards, ammonia purity, launch vehicle ammonia verification.
Технические детали
- Технический комитет
- ISO/TC 20/SC 14 - Space systems and operations
- SKU
- ISO 15859-11:2004
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