We will be carrying out essential maintenance activity on this website on Saturday 1st August between 0600 and 1300 UK time. You might experience some brief interruption or loss of some functionality. We apologise for any inconvenience this may cause.

PNW 105-1036 ED1: Unmanned aircraft systems -- General requirements and test methods for the attachable hydrogen cylinders of gaseous hydrogen fuel cell powered UAV

Scope

This document specifies the fixed performance of detachable hydrogen containers for hydrogen UAVs. It applies to the fixed performance regulations for the safety and integrity of hydrogen containers, which are key components of hydrogen UAVs, to ensure safe flight and intended performance.

Purpose

This document is applied to the locking performance and requirements of special high pressure cylinders. It aims at preventing the occurrence of conditions where safe flight cannot be finished due to the power loss of fuel cell drones caused by their imprecise locking because they are directly linked to the improvement in flight safety.

Comment on proposal

Required form fields are indicated by an asterisk (*) character.


Please email further comments to: admin.start@bsigroup.com

Follow standard

You are now following this standard. Weekly digest emails will be sent to update you on the following activities:

You can manage your follow preferences from your Account. Please check your mailbox junk folder if you don't receive the weekly email.

Unfollow standard

You have successfully unsubscribed from weekly updates for this standard.

Error