Nesmith Cougar I

Sheet metal, tube, wood and fabric mono-plane with folding wing powered by Cont. 85-hp engine.

specifications
 
powerplant
propeller
length
height
wing span
wing area
seats
empty weight
 useful load
gross weight
fuel capacity
range		 Cont. 85 HP Range65-125
x
18.9 ft
5.5 ft
20.5 ft
82.5 sq. ft
2
624 lb
x
1250 lb
25gal
 600n.m

performance

takeoff distance, ground roll
rate of climb
max speed
cruise speed
landing distance, ground roll
 service ceiling		 800 ft
 1000fpm
 195mph
 135mph
 700 ft
 16,000 ft

limiting and recommended speeds

design manoeuvring speed (Va)
never exceed speed (Vne)
stall, power off (Vsl)
landing approach speed 		x
x
 53mph
x

All specifications are based on manufacturer's calculations