Table of Contents

1. SCOPE
2. REFERENCES
3. GENERAL
4. FCS INTEGRATION WITH THE AIRCRAFT
5. SAFETY
6. PROOF AND BURST
7. MATERIAL COMPATIBILITY
8. AFFECTED CERTIFICATION REQUIREMENTS
9. ENVIRONMENTAL
10. GASEOUS H2 STORAGE AND DISTRIBUTION
11. OXIDANT SUPPLY AND DISTRIBUTION
12. FUEL CELL MODULE CONSIDERATIONS
13. BALANCE OF PLANT CONSIDERATIONS
14. THERMAL MANAGEMENT CONSIDERATIONS
15. CONTROLLER / SYSTEM INTERFACE CONSIDERATIONS
16. SENSORS
17. ELECTRICAL POWER CONDITIONING
18. POWER STORAGE
19. ELECTRICAL POWER INTERFACE
20. MAINTENANCE
21. NOTES

Abstract

Describes the technical requirements for the safe integration of gaseous hydrogen fueled Proton Exchange Membrane (PEM) Fuel Cell Systems (FCS) within the aircraft.

General Product Information

Published
Document Type	Standard
Status	Current
Publisher	SAE International
Pages
ISBN