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

Parazoom Trio-Star Delta

From Wikipedia, the free encyclopedia

Parazoom Trio-Star Delta
Role Ultralight trike, bicycle and powered parachute
National origin Germany
Manufacturer Parazoom
Status In production (2013)

The Parazoom Trio-Star Delta is a German ultralight trike, bicycle and powered parachute, designed and produced by Parazoom of Rheine. The aircraft is supplied as a complete ready-to-fly-aircraft.[1]

YouTube Encyclopedic

  • 1/3
    Views:
    1 156
    3 717
    5 991
  • VANGUARD V2.0
  • Kohler ultralight engine
  • Briggs & Stratton Paramotor Conversion

Transcription

Design and development

The Trio-Star was designed to comply with the Fédération Aéronautique Internationale microlight category, including the category's maximum gross weight of 450 kg (992 lb). It features a Bautek Pico cable-braced hang glider-style high-wing, weight-shift controls, a single-seat open cockpit without a cockpit fairing, adjustable tricycle landing gear and a single engine in pusher configuration. It can also be equipped with a paraglider wing or ridden as a bicycle, with the appropriate options fitted.[1]

The aircraft is made from welded steel tubing, in its "Delta" configuration it is fitting with a double surface hang glider wing covered in Dacron sailcloth. The 9.7 m (31.8 ft) span wing is supported by a single tube-type kingpost and uses an "A" frame weight-shift control bar. The powerplant is a V twin-cylinder, air-cooled, four-stroke 33 hp (25 kW) Briggs & Stratton Vanguard engine. The landing gear has an adjustable track width, depending on the application and wing used. The aircraft has an empty weight of 91 kg (201 lb) and carries a full fuel load of 15 litres (3.3 imp gal; 4.0 US gal).[1]

Specifications (version)

Data from Bayerl[1]

General characteristics

  • Crew: one
  • Wingspan: 9.7 m (31 ft 10 in)
  • Wing area: 12.7 m2 (137 sq ft)
  • Empty weight: 91 kg (201 lb)
  • Fuel capacity: 15 litres (3.3 imp gal; 4.0 US gal)
  • Powerplant: 1 × Briggs & Stratton Vanguard twin cylinder, air-cooled, four stroke engine, 25 kW (33 hp)
  • Propellers: 3-bladed composite

References

  1. ^ a b c d Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 218. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X

External links

This page was last edited on 10 December 2022, at 03:38
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.