AERODESIGN
Aerodesign Desenvolvimentos Aeronáuticos Ltda
Rua Nicarágua, 39 - 5ºandar - Sion
CEP 30.320-050 - Belo Horizonte (MG)
Phone (031) 285.2657
PEGASUS Technical specifications
wing span
32 ft
stall velocity
33/35 mph
total length
21 ft
manouvering velocity-Va
66/70 mph
wing surface
167 ft
glide velocity
55/58 mph
aerodynamic mean chord
5.2 ft
cruise velocity (85% Power)
100/110 mph
cabin width
42 in
maximum velocity
110/120 mph
number of seats
2, side by side
never exceed velocity
140 mph
empty weight
590 to 660 Lbs
climb rate
600/900 fpm
maximum gross weight
1100 Lb
glide ratio
12:1
usefull load (including the fuel)
507 Lb
take-off distance
200/280 ft
fuel capacity
24 gal.
landing distance
200/250 ft
available engines
ROTAX 582 or 912
flight endurance
6 hours
construction characteristics
wings: aluminum alloy 2024T3 structure
maximum range
600/900 NM
fuselage, tail, ailerons, flaps and main gear
composite materials and processes
load factors: operational limits / structural limits
+4, -2g
+6, -3g
photo
.
.
performance data, first value related to Rotax 582 engine and second to Rotax 912.
performance data realted to sea level operation.
data provided by Aerodesign Desenvolvimentos Aeronáuticos Ltda at Mar/97.
© 1998 Cláudio Amaral