INIS
design
100%
propulsion systems
100%
range
100%
power systems
100%
aircraft
100%
configuration
62%
rotors
37%
power
25%
geometry
25%
lithium
12%
air
12%
capacity
12%
occupants
12%
market
12%
voltage
12%
internal market
12%
dimensions
12%
mobility
12%
speed
12%
architecture
12%
pitches
12%
passengers
12%
propulsion
12%
solids
12%
computerized simulation
12%
electric motors
12%
energy density
12%
Engineering
Power Engineering
100%
Aircraft
100%
Design
100%
Wings
100%
Rotors
42%
Battery (Electrochemical Energy Engineering)
42%
Power Source
28%
Lithium Battery
14%
Final Configuration
14%
Energy Density
14%
Electrical Power System
14%
Computer Simulation
14%
Air Mobility
14%
Blade Geometry
14%
Fields
14%
Cruise Condition
14%
Propeller Geometry
14%
Preliminary Design
14%
Early Stage
14%