Schempp-Hirth Nimbus-2

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The Schempp-Hirth Nimbus-2 is an Open Class glider built by Schempp-Hirth during the 1970s. The Nimbus-2 first flew in April 1971 and a total of over 240 examples of all subtypes have been built until the beginning of the 1980s.

Loosely based on the original Nimbus HS-3 prototype, the production version that eventually surfaced as the Nimbus-2 was a very different glider with many improvements over the problematic prototype. The wing was shortened to 20.3 metres and was built in four sections to make it easier to rig and transport. It received Schempp-Hirth air brakes fitted in the upper surfaces and a tail braking-parachute, plus camber-changing flaps. It had an all-flying T-tail similar to the Standard Cirrus as well as the general layout of its fuselage.

The Nimbus-2 was successful in competitions, twice winning the Open Class in World Gliding Championships: Göran Ax (Sweden) in 1972 and George Moffat (USA) in 1974. It was also popular with record-seekers. Bruce Lindsey Drake, David Napier Speight and Sholto Hamilton "Dick" Georgeson jointly set a World Goal and Free Distance record of 1,254 km in New Zealand in 1978, Doris Grove a feminine Out and Return record of 1,127 km in 1981, Yvonne Loader a feminine Height Gain record of 10212 m in 1988, and Joan Shaw a feminine Distance record of 951.43 km in 1990, all flying Nimbus-2. At it's time several national and world records were held by Nimbus-2M's in the FAI motorglider category. In 1979 Klaus Holighaus, the glider's designer, completed the first 1,000 km triangle in Germany flying a Nimbus-2.

The Nimbus-2 was succeeded by the Schempp-Hirth Nimbus-3.

Variants

* Nimbus-2
* Nimbus-2B - with a fixed incidence horizontal tail to improve pitch control behaviour
* Nimbus-2C - lighter variant with higher maximum certified flight mass, new trailing-edge combined airbrakes-flaps derived from the Glasflügel 303 Mosquito in place of the upper surface air brakes, and carbon-fibre wings and tailplane. Several other improvements took place during the production run without changes to the type designation.
* Nimbus-2CS - single example (serial number 192) with reduced fuselage weight, an increased span of 23.5 m, an enlarged rudder and several other modifications.
* Nimbus-2M - Self-launching version with a retractable engine. It is based on the Nimbus-2 (not 2b) but the wing is 15 cm further aft on the fuselage to make up for the C of G shift induced by the weight of the engine (7 built)

pecifications (Nimbus 2b)

aerospecs
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crew=One
capacity=120 kg - 200 kg (264 lb - 440 lb) water ballast
length m=7.33
length ft=24
length in=1
span m=20.30
span ft=66
span in=7
swept m=
swept ft=
swept in=
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rot dia m=
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dia m=
dia ft=
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width m=
width ft=
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height m=1.45
height ft=4
height in=9
wing area sqm=14.4
wing area sqft=155
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio= 28.6
wing profile= FX 67-K-170 / FX 67-K-150
empty weight kg=345
empty weight lb=759
gross weight kg=580
gross weight lb=1,276
lift kg=
lift lb=

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max speed kmh=270
max speed mph=170
max speed mach=
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range km=
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endurance h=
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ceiling m=
ceiling ft=
glide ratio= ca. 47.5
climb rate ms=
climb rate ftmin=
sink rate ms= 0.49
sink rate ftmin= 96

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References

*Thomas F, Fundamentals of Sailplane Design, College Park Press, 1999
*Simons M, Segelflugzeuge 1965-2000, Eqip, 2004
* [http://www.sailplanedirectory.com/ Sailplane Directory]
* [http://www.rcawsey.fsnet.co.uk/nimbus2.htm Production list]
* [http://www.schempp-hirth.com/ Schempp-Hirth homepage]