STEMME S12
It has been 30 years now since the first Stemme S10 was launched, and in that period until today more than 270 S10 and S12 aircraft have been delivered to customers worldwide.
The Twin Voyager S12 has been presented to the market two years ago. The S12 is a further and comprehensive evolution of the S10 which was already successful in its own right. It was a successful introduction, its production capacity is booked well into 2018.
The new S12 will be equipped with a new lighting system using LED technology. This is not only a design feature, it also enhances flight safety. The LED light strip in the nose cone is linked to the aircraft collision avoidance system and reacts with an adapted signal according to the traffic situation.
It offers aerodynamic improvements by integrating the LED lights into improved winglets. And it also enhances the aesthetic aspect of the aircraft.
Furthermore, as another step in our increased product offering we introduce a full glass cockpit, i.e. a Garmin avionics panel with two G3X touch panels, Garmin autopilot, digital engine control monitoring and much more.
These new features will be available for delivery from the second quarter of 2018 onwards.
We are able to offer this continuous product enhancements because not only do we strongly believe in but more importantly we apply the excellence of German engineering. Along with excellence in manufacturing this provides our customers today with an aircraft giving unparalleled flying experience and quality that speaks for itself.
The Stemme Twin Voyager S12 is a powerful single piston engine aircraft as well as an elegant high performance glider. It is truly two aircraft in one.
As you can see, with our latest and newest features for the S12, Stemme is above it all. That describes well that Stemme stands for innovative engineering; high quality manufacturing; unrelenting attention to detail; passionate about our products; offering our customers a unique flying experience in aircraft with which our customers can be above it all.
Junkers Rescue Equipment
The Magnum Light Speed Softpack is a rocket activated rescue system, designed to save lives of the crew of a microlight with a MTOW up to 475 kg. The device guarantees very fast opening of the canopy, even in low altitude and minimum speed 100 km/h. There are situations in which a rescue system cannot provide a rescue of 100 %.
C42 C
Agile and maneuverable
MTOW: 560 kg
Approval as: LTF-UL 2019 / BCAR S
Features of the C42 C
The IKARUS C42C is an innovative development based on the proven IKARUS C42 series
– high-performance EH airfoil with GRP sandwich-reinforced leading edge
– standard wind tunnel and CFD flow simulation optimized winglets
– better control comfort with Spades and Flettner rudder
– better engine cooling due to lightweight tubular frame engine support made of high-strength performance steel
– improved cockpit seals through redesign of the windscreens and door integration
– aerodynamic optimisation of the fuselage – landing flap transition through gap claddings
Areas of application
Used for flight schools, as a touring aircraft, as a tow plane. Can be equipped with a Rotax 912iS engine and a Rotax 914 Turbo. Optional with floats or skis.
Standard equipment for C42 C
80 HP Rotax engine | rescue system | stainless steel exhaust system | hydraulic disc brakes with parking brake | comfortable and effective cabin heating | carburettor preheating | airbox with Naca inlet | covering with extra protective film against UV rays | inspection-friendly wing and cowling locks | large luggage compartment opening | cabin locks with new high-security designer door handles | adjustable air inlets in both doors | incl. basic flight instruments, engine instruments, decorative strips | digital, precisely readable tachometer with engine time recording | can also be equipped with the special version for pilots in a wheelchair
plus
– Tubular engine mount
– Spades
– Flettner-rudder
– Gap cladding between landing flaps and fuselage for reduction of turbulences
– Light winglets made of honeycomb sandwich
– Electric elevator trim with stick actuation
– Strut connection cladding
C42 C Technical data
Injection Super Bison
Engine 912 UL 912 ULS 912 iS 914 UL
Power 80 PS 100 PS 100 PS 115 PS
Cruising speed 75% 172 km/h 182 km/h 182 km/h 202 km/h
Maximum speed Vmax 188 km/h 196 km/h 196 km/h 213 km/h
Stall speed VS0 71 km/h 71 km/h 71 km/h 71 km/h
Rate of climb 4 m/s 5 m/s 5 m/s 7,5 m/s
Span width 8,71 m
Lenght 6,38 m
Height 2,20 m 2,20 m 2,20 m 2,20 m
Wing area 11,9 m² 11,9 m² 11,9 m² 11,9 m²
Max. take-off weight / MTOW 560 kg
Empty weight incl. rescue system BRS 279 kg 283 kg 291,3 kg 291 kg
Load capacity 281 kg 277 kg 268,7 kg 269 kg
Tank capacity 65 Liter
Consumption liters/hour 11 - 14 12 - 15 11 - 14 12 - 15
Range with 65 liter tank ca. 760 km
Take-off roll distance (grass) 120-140m 100-120m 100-120m 90-100m
Glide ratio 11
Data status: October 2021 – subject to change.
Technical data are partly approximate values.
C42 CS
The fastest in the IKARUS series
MTOW: 560 kg
Approval as: LTF-UL 2019
Features of the C42 CS
The IKARUS C42CS is an innovative further development based on the proven IKARUS C42C.
The well-known innovations and technical developments already implemented in our successful C42C are rounded off by the composite single-swing landing gear and is the logical further development to the standard sports aircraft.
The aerodynamically high-quality landing gear offers a significantly higher cruising speed. Thus, sporty and pleasant traveling complement each other to a perfect flying experience.
Areas of application
Wird eingesetzt für Flugschulen, als Reiseflugzeug, als Schleppflugzeug.
Kann mit einem Rotax IS Motor ausgestattet werden.
Standard equipment for the C42 CS
80 hp Rotax engine | rescue system | stainless steel exhaust system | hydraulic disc brakes with parking brake | comfortable and effective cabin heating | carburettor preheating | airbox with NACA inlet | cover with extra protective film against UV rays | inspection-friendly wing and cowling locks | large luggage compartment opening | cabin locks with new high-security designer door handles | adjustable air inlets in both doors | incl. basic flight instruments, engine instruments, decorative strips | digital, precisely readable tachometer with engine time recording | can also be equipped with the special version for pilots in a taxiing stall
plus
– Engine frame carrier
– Spades
– Flettner-rudder
– Gap fairing between flaps and fuselage
– Electric elevator trim with stick actuation
– Strut connection cladding
– Aerodynamic single swing composite landing gear
– High quality Beringer brake including parking brake
C42 CS Technical specifications
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Injection |
|
|
|
|
|
|
|
|
Power |
80 PS |
100 PS |
100 PS |
|
|
Cruising speed 75% |
184 km/h |
194 km/h |
194 km/h |
|
|
Maximum speed Vmax |
200 km/h |
208 km/h |
208 km/h |
|
|
Stall speed VS0 |
71 km/h |
71 km/h |
71 km/h |
|
|
Rate of climb |
4 m/s |
5 m/s |
5 m/s |
|
|
Wing span |
8,71 m |
|
|
|
|
Lenght |
6,38 m |
|
|
|
|
Height |
2,20 m |
|
|
|
|
Wing area |
11,9 m² |
|
|
|
|
Max. take-off weight / MTOW |
560 kg |
|
|
|
|
Empty weight incl. rescue system BRS |
281,5 kg |
285,5 kg |
293,8 kg |
|
|
Load capacity |
278,5 kg |
274,5 kg |
266,2 kg |
|
|
|
|
|
|
|
|
Tank capacity |
65 Liter |
|
|
|
|
Consumption liters/hour |
11 - 14 |
12 - 15 |
11 - 14 |
|
|
Range with 65 liter tank |
approx. 780 km |
|
|
|
|
Take-off roll distance (grass) |
120-140m |
100-120m |
100-120m |
|
|
Glide ratio |
11 |
|
|
|
BREEZER SPORT
ALUMINIUM AT IT’S BEST.
The Breezer Sport. The design complementing the proven B400/B600 series focussing on speed. The B400/B600 design philosophy had its roots in the ease of building for the homebuilder market back in the early days. Today, we can do things differently and that’s why the Breezer Sport has a totally different approach, still maintaining the famous Breezer Design Harmony. The current integration of 3D CAD/CAM systems enables us to create form factors meeting the expectations of strength and performance. Therefore, the Breezer Sport is not only an enhancement of the B400/B600. It is a completely new aircraft with totally different technology approaches.
Aluminium is our core competence so it had been a fascinating task to design a round fuselage. Thanks to advanced 3D CAD/CAM, the design with finished on a monitor rather than finding spots in the physical prototype section. As a special task, the design has to fit the current regulations for ultralights in Germany and has to be ready for new rules once they are visible by the authorities. Counter-sunk rivets support the clean design in smooth surfaces.
A special focus is the retractable landing gear. „Metal made in Germany“ and it should not be “just any” solution to do the job, it should be lightweight, safe and efficient - „Mission accomplished“. The tapered wings are new in all aspects from profile to main spar. This is now a centre spar in a centre section up to the landing gear. The wings as such are shorter and are attached to the main section left and right. To support low speed behaviour, new developed flaps provide enough lift.
The Breezer Sport is prepared to carry the Rotax-engines 912 ULS and 915 iS. The cowling is adopted to generate less drag and allow large openings for coolants or intercooler. The visual dominance in the future is the large side intake.
The Breezer Sport – Specifications at a glance:
|
|
141 HP |
|
Cruising speed (75%) |
270 km/h |
|
Maximum speed VNE* |
292 km/h |
|
Wingspan |
7,76 m |
|
Cabin width |
1,16 m |
|
Length |
6,92 m |
|
Height |
2,24 m |
|
Max. Flying weight* |
600 kg |
|
Fuel tank capacity |
120 l |
|
Maximum range |
1400 km |
C42
