JS-MD Single

Together with our main partner Jonker Sailplanes from South Africa, we fulfil key functions with regard to the European certification of the JS-MD Single. We are the type certificate holder for all JS models in Europe. Therefore, all JS aircraft with EASA type certification are manufactured under our production authorisation. In addition, all JS aircraft arriving in Europe undergo our final quality control and are prepared for handover. In this way, we ensure that all requirements are met and all necessary documentation is available.

JS-MD 1C

The JS1 Revelation

18m/21m flapped sailplane

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The JS1 Revelation is a high-performance FAI open class glider with a length of 18 and/or 21 metres.

Designed with aerodynamics, structures and pilot comfort in mind, the JS1 has quickly gained worldwide recognition for its outstanding performance and flight characteristics.

The JS1 is available either as a pure glider or with the MD-TJ 42 engine installed.

Although production has been discontinued, pristine examples of the JS1 are available all over the world.

Technical Data

Measures and Weight

Wingspan

18 m

21 m

Wing surface

11.19 m2

12.25 m2

Wing extension

29

36

Hull length

 7,16 m

 7,16 m

Rumpfhöhe

1,32 m

1,32 m

max. take-off weight

600 kg

720 kg

Tare weight

310 kg

435 kg

Surface load (max)

54 kg/m²

58,7 kg/m²

Surface load (minimum 70kg pilot weight)

35,3 kg/m²

33,8 kg/m²

Performance

Wingspan

18 m

21 m

Best glide ratio

1:53

1:60

minimum descent rate

0.5 m/s

0.48 m/s

best recomm. glide (at max. weight)

120 km/h

120 km/h

best recomm. glide (at 450 kg)

100 km/h

100 km/h

VNE Max. speed

270 km/h

270 km/h

VRA in gusty weather

203 km/h

203 km/h

JS-MD 3

The JS3 Rapture

15/18m Single seater

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The JS3 Rapture is a high-performance glider in the FAI 15 and/or 18 metre class. The JS3 is available either as a pure sailplane or with the MD-TJ 42 engine installed.

Optional 15 metre outboard wing tips transform the JS3 into a fast, manoeuvrable glider.

The standard equipment sets the JS3 apart from other gliders in its class. It has been designed for pilots with a desire for ultimate performance.

The JS3 has been proven to offer the best in performance, safety, handling and comfort.

Early on, the designers Attie Jonker and Johan Bosman thought about a new development with a 15 metre wingspan, but with more performance than usual for the class. The two saw the key to achieving significantly more performance above all in the realisation of a new fuselage. The usual wind tunnel tests were replaced by highly effective CFD analysis (computational fluid dynamics). This enables fast and efficient simulation of flows in order to calculate the forces at work and thus understand the effects on the aircraft's performance. The results achieved are extremely impressive. In addition to a significantly optimised glide ratio, uncomplicated flight behaviour (independent of the load condition), a high maximum wing loading, crash safety and cockpit ergonomics were also on the agenda.

 

The JS-MD 3 has not only been newly developed and designed by an experienced team over many thousands of hours. A new and integrated development approach also breaks new ground in production. Every aspect, every component, every function of a large or small part, the manufacturing process, the optimum material thickness and the required mould were defined and developed together. This approach is somewhat slower during the initial phase, but ultimately saves time in production and significantly increases precision. This made it possible to significantly reduce the mass of the aircraft without having to compromise on safety. Thanks to the high level of manufacturing precision, it is now possible to interchange wings, stabilisers or fuselages from different aircraft for the first time without any further adjustments. A novelty in sailplane construction. The JS-MD 3 is an aircraft with a performance above the usual 15 metre class, combined with maximum wing loading and the proven jet system from M&D Flugzeugbau. Last but not least, a very characteristic and dynamic design was created.

Technical Data

Measures and Weight

Wing span

15 m

18 m

Wing surface
8,75 m2
9,95 m2
Wing extension
25,4
32,8
Hull length
6,86 m
6,86 m
Hull height
1,22 m
1,22 m
Rumpfhöhe
max. take-off weight
525 kg
600 kg
Surface load (max)
40 kg/m2
37 kg/m2
Surface load (at least 70kg Piloteweight)
60 kg/m2
60 kg/m2

JS-MD 3 RES

The JS3 Rapture RES

15/18m Single seater

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The JS3 Rapture is a high-performance glider in the FAI 15 and/or 18 metre class. The JS3 RES is available either as a pure sailplane or with the built-in
electric solo engine/self-launch system.

Optional 15m outboard wing tips transform the JS3 RES into a fast, manoeuvrable glider.

The standard equipment sets the JS3 RES apart from other gliders in its class. It has been developed for pilots who are looking for ultimate performance.

The JS3 RES has been proven to offer the best in performance, safety, handling and comfort.

Technical Data

Measures and Weight

Wing Span

15 m

18 m

Wing surface
8,75 m2
9,95 m2
Wing extension
25,4
32,8
Hull length
6,86 m
6,86 m
Hull height
1,22 m
1,22 m
max. take-off weight
525 kg
600 kg
Surface load (max)
40 kg/m2
37 kg/m2
Surface load (at least 70kg Piloteweight)
60 kg/m2
60 kg/m2
Electric Motor
EMRAX 208
Propeller type
Technoflug KS-1C-120-R-065-S
Maximum Static thrust
90 daN
Maximum RPM
4350
Max power for take-off
40 kW
Max continuous climb power
25 kW
System weight (no batteries)
+/- 24kg (53 lbs)

Battery Specification

Battery Type
EMECTRIC BM 384
Battery configuration
96S4P
Battery Voltage
270V-400V
Usable Energy
(available energy decreases with high power settings)
3.4 – 4.2 kWh per battery
Battery weight
25kg (55.1 lbs)
Maximum number of batteries
2

Standard features for your comfort

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  • Low-noise propeller design

  • Pilot interface: a single switch controls the pylon extension and doors

  • Optional configuration with two batteries or with one battery

  • Automatic centring of the propeller after switching off

  • Opening/closing of the engine room doors with control sequencing to close the doors for both the retracted and extended position of the pylon.

     

TCDS

Approach

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