En un primer momento se consideraron dos configuraciones, ambas con un fuselaje facetado y configuración pusher, este diseño permite una fácil construcción dado el hecho que no se requieren moldes o partes de fibra de vidrio para dar formas complejas.
El contra principal es que exigía un fuselaje alargado de manera que sea estéticamente agradable, asiéndolo viable para una configuración biplaza.
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Initial Layouts
At the begining of the project two configurations was considered, both pusher with faceted fuselage, this design allow an easy construction due no molds were required or fiber glass parts in order to get some complex shapes.
The main contra was the fact that a long fuselage was required to get an aesthetic product, making her a good option for a two-seat version.
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Initial Layouts
At the begining of the project two configurations was considered, both pusher with faceted fuselage, this design allow an easy construction due no molds were required or fiber glass parts in order to get some complex shapes.
The main contra was the fact that a long fuselage was required to get an aesthetic product, making her a good option for a two-seat version.
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Requisitos / Design Goals:
Wcrew: 175 lb (79.4 Kg)
Wpayload: 15 lb (6.8 Kg)
Fuel: 10 USGal (60.2 lb / 27.3 Kg)
WE: ± 260 lb (117.9 Kg)
WTO: ± 510 lb (226.8 Kg)
VS: 50 Knos (84.4 ft/seg / 92.6 Km/h)
VSO: 40 Knos (62.5 ft/seg / 74.1 Km/h)
Vmax: ≥ 120 Knos (202.5 ft/seg / 222.2 Km/h)
Range: ≥ 350 nm (648.2 ft)
Take-off: ≤ 492 ft (150 m)
Ceiling - Operational: 10.000 ft
Ceiling - Absolute: 15.000 ft
Climb Rate: ≥ 1000 ft/min
n: + 4.4 - 2
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