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DTA-Voy
Voyageur 912 XP15
 
The Voyageur 912 XP15 is a large trike with a topless wing, designed for aerial work or long rallies. It features individual composite seas.
 
dtavoyager


The basic design is an aluminum sandwich with extra reinforcing structure. It also has a safety cable running through the sandwich. The sandwich is riveted and also bonded with aeronautical Araldite structural epoxy.
The Voyageur 912 was created for this purpose and became the first trike to be fitted with the 4-stroke 80HP Rotax 912 engine.
With the available option of the Voyageur-II’s cantilever mast, this machine can be flown with no front strut, just like its big brother.
The Voyageur II trike features a cantilever mast that is structurally strong enough to eliminate the need for the standard front tube. The basic design is an aluminum sandwich with extra reinforcing structure. It also has a safety cable running through the sandwich. The sandwich is riveted and also bonded with aeronautical Araldite structural epoxy.
The Voyageur trike utilizes only 4130 chromoly steel, a primarily stainless steel frame and aircraft grade aluminium, and is made in France.
Features that come standard on the Voyageur II include:
Full front and rear shock absorbers (rear gas shocks)
3-wheel brakes with parking brake
Cruise throttle
Large aviation tires
Padded seat covers
Rear seat head rest
Side luggage bags
Large capacity fuel tank with fuel level gauge
Instrument panel
RPM gauge, hourmeter, water temp gauge
Full electrical system
Assembled pitot system

Voyageur II  / Dynamic 16
Engine: Rotax 582

Voyageur II  / Dynamic 15/430
Engine: Rotax 582
Engine: Rotax 912 UL
Engine: Rotax 912S ULFR

Voyageur II  / Dynamic 450
Engine: Rotax 582
Empty Weight: 407 lbs
Gross Weight: 992 lbs
Useful load (582): 585 lbs
Useful load (912/S): 532 lbs
Wingspan: 33’ 5” (10.2 m)
Wing Area: 167 sq. ft (15.5 sq.m)
Length: 9’ 9” inches
Height: 12’ 5”
Fuel Capacity: 18 gallons
Cruise Speed: 56 mph
Vne: 90 mph
Rate of Climb: 700 fpm
Takeoff distance at gross weight: 262 feet
Takeoff distance over a 50' obstacle:n 590 feet
Landing distance at gross weight: 165 feet
Landing distance over a 50' obstacle: 560 feet

Voyageur 912 XP15
Empty weight: 225 kg
Wing span: 10 m
Wing area: 15.50 sq.m
Fuel capacity: 80 lt
Engine: Rotax 912, 80 hp
MAUW: 450 kg
Seats: 2
Max speed: 135 kph
Cruise speed: 100 kph
Minimum speed: 63 kph
Climb rate: 5 m/s
Fuel consumption: 10 lt/hr
Price (1998): 220 950 Fttc
 
Engine: Rotax 912S ULFR
Empty Weight: 460 lbs

 

 

 

 


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