Tornado I (Titan aircraft)

specifications
 
powerplant
propeller
length
height
wing span
wing area
seats
empty weight
 useful load
gross weight
fuel capacity
range		 x
x
18'-3"
6'-6"
20'-0"
93 sq ft
2
320 lb
x
750 lb
10 gal
250 mi

performance

takeoff distance, ground roll
rate of climb
max speed
cruise speed
landing distance, ground roll
 service ceiling		 200 ft
1500 fpm
x
 95 mph
 200 ft
 12,500 ft

limiting and recommended speeds

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

All specifications are based on manufacturer's calculations