Schempp-Hirth Nimbus-3

The Schempp-Hirth Nimbus 3 is a glider built by Schempp-Hirth.

Nimbus-3D
Role Open-class sailplane
National origin Germany
Manufacturer Schempp-Hirth
Designer Klaus Holighaus
First flight 21 February 1981
External image
Schempp-Hirth Nimbus-3, single-seat version in flight

Design and development

The Nimbus-3 uses carbon-fibre extensively and has a new wing profile compared with the Nimbus-2. It has a four-piece carbon-fibre wing with a 22.9 metre span but may be increased to 24.5 or 25.5 metres with tip extensions. The outer wing panels are slightly modified Ventus wings. When rolling at large aileron deflection, small spoiler flaps deploy at the inner wingtip to compensate for lack of rudder power. It was first flown on 21 February 1981 by its designer Dipl.-Ing Klaus Holighaus. A glide ratio of 60:1 has been claimed. The Nimbus-3T version has a sustainer engine.

Nimbus-3s took the first three places in the Open Class in the 1981 World Gliding Championships, but because of the expense of Open Class gliders there were only 12 entrants. In the 1983 World Championships it took the top six places, and it won again in the 1985 Worlds.

The Nimbus-3D is the two-seater version. First flight was in May 1986. There is a slight forward sweep of the wings. There are also a self-launched version (Nimbus-3DM) and a sustainer version (Nimbus-3DT).

The successor was the Schempp-Hirth Nimbus-4.

Specifications (Nimbus 3)

Data from Jane's All the World's Aircraft 1988-89[1]

General characteristics

  • Crew: 1
  • Length: 7.63 m (25 ft 0 in)
  • Wingspan: 22.9 m (75 ft 2 in)
Nimbus 3/24: 24.5 m (80 ft)
  • Height: 1.55 m (5 ft 1 in)
  • Wing area: 16.3 m2 (175 sq ft)
Nimbus 3/24: 16.7 m2 (180 sq ft)
  • Aspect ratio: 32.2
Nimbus 3/24: 35.9
  • Empty weight: 392 kg (864 lb)
Nimbus 3/24: 396 kg (873 lb)
  • Max takeoff weight: 750 kg (1,653 lb)
  • Water ballast: 280 l (74 US gal; 62 imp gal)

Performance

  • Stall speed: 60 km/h (37 mph, 32 kn)
Nimbus 3/24: 59 km/h (32 kn; 37 mph)
200 km/h (110 kn; 120 mph) in rough air
180 km/h (97 kn; 110 mph) on aero-tow
150 km/h (81 kn; 93 mph) on winch launch
Nimbus 3/24190 km/h (100 kn; 120 mph) in rough air
  • g limits: +5.3 -2.65
  • Maximum glide ratio: 55:1 at 95 km/h (51 kn; 59 mph)
Nimbus 3/24:58 at 95 km/h (51 kn; 59 mph)
  • Rate of sink: 0.44 m/s (87 ft/min) at 75 km/h (40 kn; 47 mph)
Nimbus 3/24: 0.41 m/s (81 ft/min) at 75 km/h (40 kn; 47 mph)
  • Wing loading: 46 kg/m2 (9.4 lb/sq ft)
Nimbus 3/24: 44.9 kg/m2 (9.2 lb/sq ft)
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See also

Aircraft of comparable role, configuration and era

Related lists

References
  1. John W.R. Taylor, ed. (1988). Jane's All the World's Aircraft 1988-89. London: Jane's Information Group. p. 628. ISBN 0-7106-0867-5.

Further reading
  • Milgram, Fred Thomas; Judah; translator; contributor (1999). Fundamentals of sailplane design (3rd ed.). College Park, MD: College Park Press. ISBN 978-0966955309.
  • Simons, Martin (2005). Sailplanes 1965-2000 (2nd revised ed.). Königswinter: EQIP Werbung und Verlag G.m.b.H. ISBN 978-3-9808838-1-8.
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