Engineering:Parazoom Trio-Star Delta
Please use PROD only on articles. It is proposed that this article be deleted because of the following concern:
If you can address this concern by improving, copyediting, sourcing, renaming, or merging the page, please edit this page and do so. You may remove this message if you improve the article or otherwise object to deletion for any reason. Although not required, you are encouraged to explain why you object to the deletion, either in your edit summary or on the talk page. If this template is removed, do not replace it. This message has remained in place for seven days, so the article may be deleted without further notice. Nominator: Please consider notifying the author/project: {{subst:proposed deletion notify|Engineering:Parazoom Trio-Star Delta|concern=WP:DEL8: No sources of notability in article or available on the web. This article is a collection of facts from a directory as its only source. These uncontroversial deletions are not opposed by the original author after notification. Relevant: WP:NOTDIRECTORY and this AfD nomination.}} ~~~~Timestamp: 20260925234452 23:44, 25 September 2026 (UTC) Administrators: delete |
| Parazoom Trio-Star Delta | |
|---|---|
| General information | |
| Type | Ultralight trike, bicycle and powered parachute |
| National origin | Germany |
| Manufacturer | Parazoom |
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]
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
External links
 |  |
