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C.P. 150 Onyx
The C.P. 150 Onyx is a single seat,
canard, open cockpit aircraft designed by Claude Piel. Construction
materials are wood & fabric. The landing gear is a fixed trigear,
and the engine is in a pusher configuration. This aircraft qualifies
as an ultralight in Canada and the United States.
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specifications
powerplant
propeller
length
height
wing span
wing area
seats
empty weight
useful load
gross weight
fuel capacity
range |
18 HP
35" dia. x
14" pitch
11.6 ft
x
24.0 ft
137.7 sq
ft
x
265 lbs
x
475 lbs
5 US gal
x |
performance
takeoff distance,
ground roll
rate of climb
max speed
cruise speed
landing distance, ground roll
service ceiling |
150ft
450fpm
70mph
60mph
100ft
x |
limiting and recommended speeds
design manoeuvring speed (Va)
never exceed speed (Vne)
stall, power off (Vsl)
landing approach speed |
x
85mph
25mph
x |
All specifications are based on manufacturer's
calculations
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