STN EN IEC 62282-4-202
Name: | STN EN IEC 62282-4-202 |
Validity: | Valid |
Number of pages: | 28 |
Language: |
EN
|
Paper: | 14,10€ |
Electronic version |
a) Only read (without ability to print and copy)
12,69€ b) Without ability to print, with ability to copy (printscreen) 14,10€ c) With ability to print and copy (printscreen) 18,33€ |
Slovak title | Technológia palivových článkov. Časť 4-202: Napájacie systémy na palivové články pre pohonné a pomocné napájacie jednotky. Bezpilotné lietadlá. Skúšobné metódy prevádzkových vlastností |
English title | Fuel cell technologies - Part 4-202: Fuel cell power systems for propulsion and auxiliary power units - Unmanned aircrafts - Performance test methods |
Release Date: | 01. 02. 2024 |
Date of withdrawal: | |
ICS: | 27.070, 49.020 |
Sorting character/National clasification code | 36 4512 |
Level of incorporation: | idt IEC 62282-4-202:2023, idt EN IEC 62282-4-202:2023 |
Official Journal | 01/24 |
Amendments | |
Replaced by: | |
Repleces: | |
Note in Official Journal: | |
Subject of the standard: | IEC 62282-4-202:2023 covers performance test methods of fuel cell power systems intended to be used to power unmanned aircrafts, including general requirements, start-up, shutdown, power output, continuous running time, electric efficiency, data transmission, warning and monitoring, environmental compatibility, etc. The scope of this document is limited to electrically powered unmanned aircrafts with a maximum take-off mass not exceeding 150 kg (i.e. level 5 or lower unmanned aircrafts (UAs)). This document applies to fuel cell power systems with a rated output voltage not exceeding 220 V DC for outdoor use. This document applies only to compressed gaseous hydrogen-fuelled fuel cell power systems. |
Preview: | Náhľad normy (PDF) |