ISO 24352:2023
Technical requirements for small unmanned aircraft electric energy systems
- Standard No.
- ISO 24352:2023
- Release Date
- 2023
- Published By
- International Organization for Standardization (ISO)
- Latest
- ISO 24352:2023
- Scope
- This document provides technical requirements and test methods for small unmanned aircraft electric energy systems (EESs). This document applies to the EES of small unmanned aircrafts (UAs) with the maximum take-off mass (MTOM) less than 25 kg corresponding to unmanned aircraft systems (UASs) at level I, II, III and IV as graded in ISO 21895:2020, and with secondary lithium batteries. This document can apply to new type of batteries to be used in the UA electric energy system in the future.
ISO 24352:2023 Referenced Document
- IEC 60529 Degrees of Protection Provided by Enclosures (IP Code) (Edition 2.1 ***Applies to French text only***)*， 2024-04-21 Update
- IEC 60950 Corrigendum 1 - Safety of information technology equipment
- IEC 62281:2019 Sécurité des piles et des accumulateurs au lithium pendant le transport (Edition 4.0)
- ISO 21384-2 Unmanned aircraft systems — Part 2: UAS components
ISO 24352:2023 history
- 2023 ISO 24352:2023 Technical requirements for small unmanned aircraft electric energy systems
