To install click the Add extension button. That's it.

The source code for the WIKI 2 extension is being checked by specialists of the Mozilla Foundation, Google, and Apple. You could also do it yourself at any point in time.

4,5
Kelly Slayton
Congratulations on this excellent venture… what a great idea!
Alexander Grigorievskiy
I use WIKI 2 every day and almost forgot how the original Wikipedia looks like.
Live Statistics
English Articles
Improved in 24 Hours
Added in 24 Hours
Languages
Recent
Show all languages
What we do. Every page goes through several hundred of perfecting techniques; in live mode. Quite the same Wikipedia. Just better.
.
Leo
Newton
Brights
Milds

Schempp-Hirth Ventus-2

From Wikipedia, the free encyclopedia

Ventus-2
Ventus 2b being winch-launched at Lasham airfield
Role 15 metre-class and 18 metre-class sailplane
National origin Germany
Manufacturer Schempp-Hirth
First flight 1994
Number built 627

The Schempp-Hirth Ventus-2 is a sailplane produced by Schempp-Hirth since 1994. It replaced the highly successful Schempp-Hirth Ventus.

Design and development

The Ventus-2a and 2b are 15 metre sailplanes. The 'a' version has a narrow fuselage and the wider fuselage version is called the 2b. Winglets are used with these models. The 18 metre span Ventus-2c was introduced in 1995 and was almost an entirely different aircraft with a different fuselage and wings, but it has the option of shorter tips with winglets to fly as a 15-metre sailplane.

From 2003 the Schempp-Hirth Discus-2 fuselage was used for all versions, which now have the designations 2ax, 2bx and 2cx. Flight tests in 1996 showed that the 15 metre version had a glide angle of 46:1 but only after considerable work on sealing gaps and by using turbulators.

The narrow fuselage Ventus-2a has been highly successful in competitions with consecutive World Championship wins from 1995 to 2003. A narrow fuselage version with an 18-metre span, the Ventus 2cxa has also been built.

Some Ventus-2c and 2cx are fitted with small Solo 2350 sustaining engines (turbos) and are designated with a T suffix, while some are self-launching with a more powerful Solo 2625 and have the suffix 'M'. The 2cT climbs at up to 0.9 m/s (177 ft/min) and the 2cM at over 3 m/s (590 ft/min). Ranges for the powered versions in saw-tooth operation are 370 km (230 mi) and 840 km (520 mi) respectively. The 2cxa has been designed to take a jet engine. A small number of Ventus 2 were fitted with the front electric sustainer.

Production of the 2a and 2b has reached 168 aircraft, while the 2c, 2cT, and 2CM have reached 459.

A replacement model, the Ventus 3, first flew on 29 January 2016 and serial production started in April 2016.

Specifications (Ventus-2cx with 15 metre wings)

General characteristics

  • Crew: One
  • Capacity: 200 kg (440 lb) water ballast
  • Length: 6.81 m (22 ft 4 in)
  • Wingspan: 15.00 m (50 ft 9 in)
  • Height: 1.30 m (4 ft 3 in)
  • Wing area: 9.7 m2 (104 sq ft)
  • Aspect ratio: 23.3
  • Empty weight: 290 kg (640 lb)
  • Gross weight: 525 kg (1,155 lb)

Performance

  • Maximum speed: 285 km/h (180 mph, 160 kn)
  • Maximum glide ratio: 46
  • Rate of sink: 0.51 m/s (100 ft/min)

See also

Related lists

References

This page was last edited on 8 September 2023, at 23:30
Basis of this page is in Wikipedia. Text is available under the CC BY-SA 3.0 Unported License. Non-text media are available under their specified licenses. Wikipedia® is a registered trademark of the Wikimedia Foundation, Inc. WIKI 2 is an independent company and has no affiliation with Wikimedia Foundation.