avia.wikisort.org - GliderThe 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.
German single-seat motor glider, 1981
DG-400 |
 |
Role |
18 metre class sailplane Type of aircraft |
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
- 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)
- 50 l (13 US gal; 11 imp gal) with optional tanks in lieu of water ballast
- 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
- 140 km/h (76 kn; 87 mph) max
- Stall speed: 63 km/h (39 mph, 34 kn)
- Never exceed speed: 270 km/h (170 mph, 150 kn) in smooth air
- 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
- Range: 400 km (250 mi, 220 nmi) level flight
- 750 km (400 nmi; 470 mi) cruise/soar
- Service ceiling: 5,000 m (16,000 ft)
- g limits: +6 -4
- Maximum glide ratio: 45 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 kW/kg (0.0433 hp/lb)
References
- 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.
External links
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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