Quasar Tramp
It is proposed that this article be deleted because of the following concern:
If you can address this concern by improving, copyediting, sourcing, renaming, redirecting, 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. The article may be deleted if this message remains in place for seven days, i.e., after 21:33, 4 October 2026 (UTC). Find sources: "Quasar Tramp" – news · newspapers · books · scholar · JSTOR Nominator: Please consider notifying the author/project: {{subst:proposed deletion notify|Quasar Tramp|concern=[[WP:DEL8]]: No sources of [[WP:N|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 [[User talk:Ahunt#Proposed deletion of Airborne Redback|not opposed by the original author]] after notification. Relevant: [[WP:NOTDIRECTORY]] and [[Wikipedia:Articles for deletion/Ozone Peak|this AfD nomination]].}} ~~~~ |
 | This article relies on a single source. (June 2025) |
| Tramp | |
|---|---|
| General information | |
| Type | Hang glider |
National origin | Czech Republic |
| Manufacturer | Quasar |
| Status | Production completed |
The Quasar Tramp is a Czech high-wing, single-place, hang glider that was designed and produced by Quasar of Dolní Bečva. Now out of production, when it was available the aircraft was supplied complete and ready-to-fly.[1]
Design and development
[edit]The Tramp was designed as a simple leisure wing available in just one size. It is made from aluminum tubing, with the single-surface wing covered in Dacron sailcloth. Its 9.8 m (32.2 ft) span wing is cable braced from a single kingpost. The nose angle is 120°, wing area is 16.2 m2 (174 sq ft) and the aspect ratio is 5.9:1. Pilot hook-in weight range is 55 to 95 kg (121 to 209 lb).[1]
Specifications (Tramp)
[edit]Data from Bertrand[1]
General characteristics
- Crew: one
- Wingspan: 9.8 m (32 ft 2 in)
- Wing area: 16.2 m2 (174 sq ft)
- Aspect ratio: 5.9:1