Caratteristiche Tecniche |
 |
|
Compatto, leggero, potente. |
| |
 |
|
System Composition |
Power/Capacity |
| |
Motor |
(65kWe) |
Electronics (Inverter + DC/DC) |
(75kWe) |
Aux Lithium Battery |
(7,5kWhe) |
Hydrogen fuel cell |
(60kWe) |
H2 line and valve |
|
Compressor |
(12kWmax) |
H2 reservoir |
(75l x 350atm) |
|
| |
Systems Layout |
 |
|
|
| |
Hi Performance PEM Fuel Cells |
-
60kW Total Power
-
More than 1kW/kg Power Density
-
Special Pneumatic circuit for Altitude Compensation
-
Avionics Integrated Cooling System
|
|
 |
|
| |
Hi Pressure Hydrogen Reservoir |
|
| |
Innovative Electric Motor |
Manufactured by:
 |
|
 |
|
| |
Electronic Flight Information System |
Manufactured by:
 |
|
 |
|
|
