BS ISO 24352:2023
$142.49
Technical requirements for small unmanned aircraft electric energy systems
Published By | Publication Date | Number of Pages |
BSI | 2023 | 28 |
PDF Catalog
PDF Pages | PDF Title |
---|---|
2 | National foreword |
7 | Foreword |
9 | 1 Scope 2 Normative references 3 Terms and definitions |
10 | 4 Abbreviated terms 5 System requirements 5.1 General |
12 | 5.2 Performance 5.2.1 Output control |
13 | 5.2.2 Actuation time 5.2.3 Shutdown time 5.2.4 Rated output power 5.2.5 Discharge capacity |
15 | 5.2.6 Cycle life 5.2.7 Operational cycle life |
16 | 5.2.8 Recoverable hovering capacity after high temperature storage 5.3 Information and alert 5.3.1 Requirements |
17 | 5.3.2 Test method and acceptance criteria 5.4 Energy management and electrical protection functions 5.4.1 Charge state of charge (SOC) calculation 5.4.2 Discharge SOC calculation |
18 | 5.4.3 Over voltage protection 5.4.4 Under voltage protection |
19 | 5.4.5 Over temperature protection 5.4.6 Over current protection |
20 | 5.4.7 Overload protection 5.4.8 Short-circuit protection |
21 | 5.5 Structure 5.5.1 Requirements 5.5.2 Test method and acceptance criteria 5.6 Electrical shock 5.6.1 Requirements 5.6.2 Test method and acceptance criteria 5.7 Connector(s) 5.7.1 Requirements 5.7.2 Test method and acceptance criteria 5.8 Enclosure protection requirements |
22 | 5.9 Environmental adaptability 5.9.1 High temperature and humidity storage 5.9.2 Temperature shock 5.9.3 Low pressure |
23 | 5.9.4 Salt spray 5.9.5 Drop test |
24 | 5.9.6 Vibration test 6 Test environment 6.1 Normal test atmospheric conditions 6.2 Charging method |
25 | 6.3 Discharging method 7 Identification, packaging, transportation and storage 7.1 Identification 7.2 Packaging, transport and storage |
27 | Bibliography |