Rahul Sharma (Editor)

Glaser Dirks DG 400

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Top speed
  
270 km/h

Length
  
7 m

Manufacturer
  
DG Flugzeugbau

Wingspan
  
17 m

Introduced
  
1981

Glaser-Dirks DG-400 GlaserDirks DG400 Untitled Aviation Photo 2242993 Airlinersnet

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.

Contents

Glaser-Dirks DG-400 saleplane GlaserDirks DG 400 pilots aviation flying pilotspaceeu

Development

Glaser-Dirks DG-400 DG400

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.

Glaser-Dirks DG-400 GlaserDirks DG400 Untitled Aviation Photo 2242993 Airlinersnet

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.

Glaser-Dirks DG-400 SSUKDG400

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.

Glaser-Dirks DG-400 httpsuploadwikimediaorgwikipediacommonsthu

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

General characteristics

Glaser-Dirks DG-400 GlaserDirks DG400 Photos AirplanePicturesnet

  • Crew: 1
  • Length: 7 m (23 ft 0 in)
  • Wingspan: 17 m (55 ft 9 in)
  • Height: 1.4 m (4 ft 7 in)
  • Wing area: 10.57 m2 (113.8 sq ft)
  • Aspect ratio: 27.3
  • Airfoil: root:Wortmann FX-67-K-170-17; tip Wortmann FX-60-K-126
  • Empty weight: 305 kg (672 lb)
  • Max takeoff weight: 460 kg (1,014 lb)
  • Fuel capacity: 20 l (5.3 US gal; 4.4 imp gal)
  • Water ballast: 90 l (24 US gal; 20 imp gal)
  • Powerplant: 1 × Rotax 505 two-stroke retractable pylon mounted air-cooled piston engine, 32 kW (43 hp)
  • Propellers: 2-bladed Hoffman fixed pitch propeller, 1.29 m (4 ft 3 in) diameter
  • Performance

  • Cruise speed: 130 km/h (81 mph; 70 kn) economical
  • Stall speed: 63 km/h (39 mph; 34 kn)
  • Never exceed speed: 270 km/h (168 mph; 146 kn) in smooth air
  • Range: 400 km (249 mi; 216 nmi) level flight
  • Service ceiling: 5,000 m (16,000 ft)
  • g limits: +6 -4
  • Maximum glide ratio: 47 at 110 km/h (59 kn; 68 mph)
  • Rate of climb: 3.90 m/s (768 ft/min) at 80 km/h (43 kn; 50 mph)
  • Rate of sink: 0.5 m/s (98 ft/min)
  • Wing loading: 43.5 kg/m2 (8.9 lb/sq ft)
  • Power/mass: 0.0714 kg/kW (0.0433 hp/lb)
  • References

    Glaser-Dirks DG-400 Wikipedia