Caspar C 17

Length
5.1 m
Flat Wing Span
12 m
Height
1.9 m
Flat Wing Area
15.6 m²
Flat Wing Aspect Ratio
9.2
Max Speed
110 km/h
Max Ceiling
3500 m
Number of Engines
1
Aircraft Engine
First Flight
1924-01-01
Maximum Range
200 km

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Aircraft Weight Variants

Aircraft Maximum Range (km)
Caspar C 17 200

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All data (18 fields)
Name
Caspar C 17
Manufacturer
Caspar-Werke
Description
The Caspar C 17 was a mid-1920s German, low power, two seat ultralight aircraft with a cantilever wing of unusually high aspect ratio, flexibly attached to the fuselage to moderate gust effects.
First Flight
1924-01-01
Designer
Ernst Ritter von Loessel
Length (m)
5.1
Height (m)
1.9
Max Speed (km/h)
110
Max Ceiling (m)
3500
Endurance (h)
2
National Origin
Germany
Powerplant Description
1 × ABC Scorpion air-cooled flat twin, 22 kW (30 hp) each
Wikipedia Article (URL)
en.wikipedia.org/wiki/Caspar_C_17
Flat Wing Span (m)
12
Flat Wing Area (m²)
15.6
Flat Wing Aspect Ratio
9.2
Aircraft Engine
ABC Scorpion
Number of Engines
1