The DTA Voyageur is a French
ultralight trike, designed by Jean-Michel Dizier and produced by
DTA sarl of
Montélimar. The aircraft is supplied complete and ready-to-fly.[1][2]
The aircraft is made from bolted-together
aluminum tubing, with its double surface wing covered in
Dacron sailcloth. When fitted with a
DTA Dynamic 450 wing it has a span of 10.20 m (33.5 ft), supported by a single tube-type
kingpost and uses an "A" frame weight-shift control bar. The powerplant is a twin cylinder, liquid-cooled,
two-stroke,
dual-ignition 64 hp (48 kW)
Rotax 582 engine or the four cylinder, air and liquid-cooled,
four-stroke,
dual-ignition 100 hp (75 kW)
Rotax 912S engine.[1][2]
Model with a 64 hp (48 kW)
Rotax 582 engine and
DTA Dynamic 15 wing. The aircraft has an empty weight of 177 kg (390 lb) and a gross weight of 400 kg (882 lb), giving a useful load of 223 kg (492 lb). With full fuel of 70 litres (15 imp gal; 18 US gal) the payload is 173 kg (381 lb).[1][2]
Voyageur 912 S Dynamic 450
Model with a 100 hp (75 kW)
Rotax 912S engine and
DTA Dynamic 450 wing. The aircraft has an empty weight of 209 kg (461 lb) and a gross weight of 450 kg (992 lb), giving a useful load of 241 kg (531 lb). With full fuel of 75 litres (16 imp gal; 20 US gal) the payload is 191 kg (421 lb).[1][2]
Voyageur II 582 Dynamic 15/430
Improved model with a 64 hp (48 kW)
Rotax 582 engine and
DTA Dynamic 15/430 wing. The aircraft has an empty weight of 196 kg (432 lb) and a gross weight of 430 kg (948 lb), giving a useful load of 234 kg (516 lb). With full fuel of 75 litres (16 imp gal; 20 US gal) the payload is 180 kg (397 lb).[1]
Voyageur II 912 S Dynamic 450
Improved model with a 100 hp (75 kW)
Rotax 912S engine and
DTA Dynamic 450 wing. The aircraft has an empty weight of 226 kg (498 lb) and a gross weight of 450 kg (992 lb), giving a useful load of 224 kg (494 lb). With full fuel of 75 litres (16 imp gal; 20 US gal) the payload is 170 kg (375 lb).[1][2]