DSF/ISO/FDIS 24352
Technical requirements for small unmanned aircraft electric energy systems
inactive
| Organization: | DS |
| Status: | inactive |
| Page Count: | 27 |
| ICS Code (Aircraft and space vehicles in general): | 49.020 |
scope:
This document provides technical requirements and test method 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 25kg corresponding to UAS at Level I, II, III and IV as graded in ISO 21895:2020, and with secondary lithium batteries. New type of batteries to be used in the UA electric energy system in the future, shall be considered in later versions of this document.
Document History
May 10, 2023
Technical requirements for small unmanned aircraft electric energy systems
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...
Technical requirements for small unmanned aircraft electric energy systems
This document provides technical requirements and test method for small unmanned aircraft electric energy systems (EESs). This document applies to the EES of small unmanned aircrafts (UAs) with the...
DSF/ISO/FDIS 24352
Technical requirements for small unmanned aircraft electric energy systems
This document provides technical requirements and test method for small unmanned aircraft electric energy systems (EESs). This document applies to the EES of small unmanned aircrafts (UAs) with the...