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The Glaser-Dirks DG-400 is a single-seat self-launching motorglider that was produced by Glaser-Dirks between 1981 and 1992. It was the first self-launching motorglider with retractable engine and propeller to be produced in large numbers.

DG-400
Role 18 metre class sailplane
National origin Germany
Manufacturer Glaser-Dirks
Designer Wilhelm Dirks
First flight May 1981
Introduction 1981
Number built 290
Developed from Glaser-Dirks DG-200

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. 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, with a user-friendly engine control unit, made the DG-400 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.


Specifications (17 metre wings)


Data from [1]

General characteristics

50 l (13 US gal; 11 imp gal) with optional tanks in lieu of water ballast

Performance

140 km/h (76 kn; 87 mph) max
190 km/h (100 kn; 120 mph) in rough air
190 km/h (100 kn; 120 mph) on aero-tow
130 km/h (70 kn; 81 mph) on winch launch
750 km (400 nmi; 470 mi) cruise/soar

References


  1. John W.R. Taylor, ed. (1988). Jane's All the World's Aircraft 1988-89. London: Jane's Information Group. pp. 620–621. ISBN 0-7106-0867-5.



На других языках


[de] Glaser-Dirks DG-400

Die Glaser-Dirks DG-400, ein selbststartendes Segelflugzeug basierend auf der DG-202, wurde von Wilhelm Dirks entworfen und hatte den Erstflug am 1. Mai 1981. Sie kann mit 15 m Flügelspannweite oder mit optionalen Flügelenden, welche die Spannweite auf 17 m erhöhen, geflogen werden. Die Innenflügel der DG-400 sind aus CFK, die Außenflügel aus GFK, der Rumpf aus GFK mit CFK im Bereich des Triebwerks. Das Triebwerk, ein Rotax 505 mit 32 kW, wird mit einem elektrischen Spindelmotor aus- und eingefahren.[2]
- [en] Glaser-Dirks DG-400

[fr] Glaser-Dirks DG-400

Le Glaser-Dirks DG-400 est un motoplaneur monoplace fabriqué par Glaser-Dirks entre 1981 et 1990. Il a été le premier motoplaneur à dispositif rétractable produit à grande échelle.



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