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BS ISO 25013 ISO 25013 Unmanned aircraft systems. General requirements and test methods for the attachable hydrogen cylinders of gaseous hydrogen fuel cell powered UAS

Source:
ISO
Committee:
ACE/20 - Uncrewed Aircraft Systems
Categories:
Hydrogen technologies | Aerospace engines and propulsion systems
Comment period start date:
Comment period end date:
Number of comments:
0

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Scope

This document specifies the required performance of attachable hydrogen cylinders for HFC UAS with power pack hydrogen fuel cell systems. This document specifies the minimum safety, performance, and integrity requirements for attachable hydrogen cylinders, which are key components of hydrogen fuel cell powered unmanned aircraft systems (HFC UAS), to ensure safe flight and intended performance. It is applicable only to systems in which the hydrogen fuel cell power generation system is unitized as a power pack.

Please see draft for Figure 1 — Typical HFC UAS Power pack configuration showing unitized assembly design

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