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| Aircraft
Da-24 MagicONE |
The
Da-24 MagicOne is
born from the synthesis of years of job and experiences for others company.
The project is developed
around a
system that allows the total industrialization of the aircraft. The
idea of the construction of this aircraft is given by the
necessity
to have available an airplane to test the engine
that we are building, which it foresees the beginning of tests within
2010. |
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Specification
& Description
The
Da-24 is a traditional
aircraft in the forms and in the
structures,
while is being inclined in the aerodynamics, with a
fuselage to recovery
of pressure and low coefficient of aerodynamic
resistance.
The
strong
point is the
wing, it has varying laminar profile with plant tapered, and the adoption of an integrated fixed slat in the profile for
around 70% of
the wing, fowler flap and ailerons to high efficiency.
All of
this
allows a low stall speed and a maximum speed remarkable.
Therefore a cruise aircraft, excellent for aerial job. |
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| Aircraft Dimension |
|
| Wing
Span |
29.5
ft (9.00
m) |
| Overall
Length |
23.6
ft (7.20
m) |
| Overall
Height |
7.5
ft (2.30
m) |
| Maximum
Gross Weight |
990
lbs (450
kg) |
| Standard
Empty Weight |
615
lbs (280
kg) |
| Fuel
Capacity (Useable) |
21
gal (95
l) |
| Cabin
Width at Shoulders |
46
inch (117
cm) |
| Performance |
|
All
performance data is
based on the
"engine 100 hp" configuration |
|
| Takeoff
Distance |
215
ft (65 m) |
| Climb
Rate |
1400
fpm (7 m/s) |
| Max
Speed |
130
kts (240 km/h) |
| Cruise
Speed |
122
kts (225 km/h) |
| Economic
Cruise Speed |
100
kts (185 km/h) |
| Stall
Speed |
27
kts (50 km/h) |
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