DG-400
A 17-metre span DG-400
Role	18 metre class sailplane
National origin	Germany
Manufacturer	Glaser-Dirks
First flight	May 1981
Number built	290

The Glaser-Dirks DG-400 is a single-seat self-launching motorglider that was produced by Glaser-Dirks between 1981 and 1990. It was the first self-launching motorglider with retractable engine and propeller to be produced in large numbers.

[edit] Development

The cost of carbon-fibre had fallen enough in the late 1970s to allow its use in the wing spars of high-performance gliders. Glaser-Dirks introduced a carbon wing variant of the DG-200 about this time. The designer, Wilhelm Dirks, realised that the span, strength and very low weight of this wing allowed for a self-launching engine to be carried in the glider without an unacceptable penalty when soaring in weak conditions. The DG-400 was created as a result. It first flew in May 1981.

The DG-400 uses the wings and most systems of the DG-202. It has a modified fuselage with a slightly enlarged tailcone and carbon fibre reinforcements to accommodate the engine, which is a relatively large unit with electric starter and electric retraction. This powerful installation, associated with a user-friendly engine control unit, ensured that the DG-400 was significantly safer and easier to operate than other self-launching gliders.

As was typical for the time, the engine, propeller and supporting pylon constitute a single unit that extends into the airflow (in more recent self-launchers the engine usually stays inside the fuselage). The type may be flown either with 15 metre or 17 metre wingtips.

The DG-400 was not aimed at competitions, but rather at leisure flying. Nevertheless, several World Gliding Records have been achieved flying this type.

[edit] Specifications (17 metre wings)

General characteristics

• Crew: One pilot
• Capacity: 90 kg (200 lb) water ballast
• Length: 7.00 m (23 ft 0 in)
• Wingspan: 17.00 m ( ft in)
• Wing area: 10.6 m² (114 ft²)
• Aspect ratio: 27.3
• Empty weight: 310 kg (680 lb)
• Gross weight: 460 kg (1,010 lb)
• Powerplant: 1 × Rotax 505, 32 kW (43 hp)

Performance

• Maximum speed: 270 km/h (170 mph)
• Range: 380 km (240 miles)
• Maximum glide ratio: 45
• Rate of sink: 0.54 m/s (106 ft/min)

[edit] References

• DG-Flugzeugbau website
• Sailplane Directory

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