Enjoy
Freedom
1:53
glide ratio
TOP PERFORMANCE, EXCELLED.
STEMME TWIN VOYAGER S12. TWO AIRCRAFT UNITED IN ONE UNBEATABLY PRECISE MACHINE.
ADVENTURE, INTEGRATED
FOLDABLE PROPELLER, TURBO-CHARGED ENGINE.
The Stemme foldable and variable pitch propeller is installed in the Stemme Twin Voyager S12 and disappears completely into the propeller dome. To start the propeller, the dome slides out and the propeller blades unfold. It takes just 5 seconds to convert from glide mode to engine mode.
CONQUER SPACE
SEPARATE BAGGAGE COMPARTMENT.
A separate baggage compartment is integrated into the fuselage. By providing space for hand luggage, the compartment significantly expands your touring options.
PREMIUM EQUIPMENT
ELECTRIC TRIM, DISCONNECTABLE AUTOPILOT.
An autopilot is part of the richly equipped cockpit. In disconnected mode it provides an extremely direct steering feeling, unbeatably immediate and sensitive. With its innovative electrical trim equipment, the Stemme Twin Voyager S12 puts the perfect tool for superlative performance into its pilot’s hands.
SHARE THE VIEW
SAFE SIDE-BY-SIDE COCKPIT, ADDITIONAL STORAGE SPACE.
The solid and safe one-piece canopy offers great panoramic views. The side-by-side alignment is ideal for sharing workloads, using the same avionics or simply for pure recreation—just as in conventional planes. The center-tunnel-fairing provides additional storage space for your smartphone, notebook and other onboard companions.
STANDARDS,
OUTNUMBERED.THE STEMME TWIN VOYAGER S12
TECHNICAL DATA.
- Weights and Dimensions
- Performance Data
- Engine
- Electrics
- Cockpit
- Airframe & Wings
- Avionics (Options)
Weights and Dimensions
- MTOM:
900 kg (1,984 lbs) - Wingspan:
25 m (82.02 ft) - Wingspan (folded):
11.4 m (37.40 ft) - Wing area:
19.95 m² (214.74 ft2) - Height:
1.75 m (5.74 ft) - Length:
8.42 m (27.6 ft)
Performance Data
- Glide ratio:
1:53* - Cruise speed up to:
259 km/h (140 kt) TAS @ 10,000 ft - Climb rate:
Better than 3,28 m/s (645 ft/min)* - Range of up to:
1,759 km (950 nm) - *to be confirmed following flight test
Engine
- Power plant:
ROTAX 914 F2/S1 Turbo - MTOP:
84,5 kw - MCP:
73,4 kw - Fuel capacity (center wing):
120 l (31.7 US gal) - Fuel consumption at 55% MCP:
13 l/h (3.4 US gal/h)
Electrics
- Solar panels
- LED lighting equipment, AVEO Starlet (ACL and position light integrated in winglets)
- USB power outlet
- 2 separated electrical systems for engine and Avionics, each supplied by a dedicated Lithium-Iron-Phosphate Battery
- Gooseneck microphone
- External power supply receptacle for ground engine start
Cockpit
- Different interior colors and premium material options with low noise ambience
- Comfort seats for pilot and co-pilot
- Tinted canopy
- Lockable windows
Airframe & Wings
- Retractable undercarriage
- 2 × 60 l fuel tanks
- Winglets with Starlet LED Lights
- Foldable wings
- Propeller Dome with integrated Collision Avoidance LED Stripe (optional)
Avionics (Options)
- Soaring computer LX9070 with digital variometer LX V8 (or optional LX V80)
- Dynon EFIS-D10A (optional)
- Dynon Autopilot (optional)
- ADS-B receiver with integrated FLARM
- Mode-S Transponder cl. 1