DA36
DIAMOND DA-36 E-Star
DIAMOND DA-36 E-Star
Aircraft
Name
DA-36 E-Star
Manufacturer
Body
Narrow
Wing
Fixed Wing
Position
Low wing
Tail
T-tail
WTC
L
Type Code
L1E
Engine
Electric
Engine Count
Single
Position
In fuselage
Landing gear
Tricycle fixed
Manufactured as
DA36
Developed by Siemens, EADS and Diamond Aircraft to reduce fuel consumption and emissions by up to 25 percent, using a serial hybrid drive that turns the aircraft's prop with a Siemens 70 kW (94 hp) electric motor, from power generated by a 40 hp (30 kW) Austro Engines Wankel rotary engine and generator, stored in batteries.
Technical Data
Wing span (metric)
16.00 m
Length (metric)
7.10 m
Height (metric)
1.70 m
Powerplant
1 x Siemens 70 kW electric motor, from power generated by a 30 kW Austro Engines Wankel rotary engine and generator.
Indicative Performance Data
Take-Off
V2
n/a
Distance
n/a
MTOW
800 kg
Initial Climb (to 5000 ft)
IAS
n/a
ROC
n/a
Initial Climb (to FL150)
IAS
n/a
ROC
n/a
Initial Climb (to FL240)
IAS
n/a
ROC
n/a
MACH Climb
MACH
n/a
ROC
n/a
Cruise
TAS
n/a
MACH
n/a
Ceiling
n/a
Range
n/a
Initial Descent (to FL240)
MACH
n/a
ROD
n/a
Descent (to FL100)
IAS
n/a
ROD
n/a
Descent (FL100 & below)
IAS
n/a
MCS
n/a
ROD
n/a
Approach
Vapp (IAS)
n/a
Distance
n/a
