Engineering:Airtime Explorer
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:Airtime Explorer|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: 20260928130334 13:03, 28 September 2026 (UTC) Administrators: delete |
| Explorer | |
|---|---|
| General information | |
| Type | Powered hang glider harness |
| National origin | Australia |
| Manufacturer | Airtime Products |
The Airtime Explorer is an Australian powered hang glider harness that was designed and produced by Airtime Products of Airlie Beach, Queensland. Now out of production, when it was available, it was supplied assembled.[1]
Design and development
When combined with a cable-braced hang glider-style wing, the single-engine pusher configuration Explorer features weight-shift controls, foot-launching and landing.[1]
The powered harness is mated to a standard hang glider wing. The wing is supported by a single tube-type king post and uses an "A" frame control bar. The engine is a two-stroke, single cylinder Radne Raket 120 of 14 hp (10 kW), and fitted with a 3.5:1 ratio reduction drive. The nylon harness mounts the engine and 5 litres (1.1 imp gal; 1.3 US gal), or optionally 10 litres (2.2 imp gal; 2.6 US gal) fuel tank. Dual retractable skids are provided to protect the propeller during take-off and landing. Electric starting and a carbon fiber folding 135 cm (53 in) propeller are standard features.[1]
Specifications (Explorer)
Data from Bertrand[1]
General characteristics
- Crew: one
- Empty weight: 23 kg (51 lb) (harness, engine, propeller only)
- Fuel capacity: 5 litres (1.1 imp gal; 1.3 US gal) or optionally 10 litres (2.2 imp gal; 2.6 US gal)
- Powerplant: 1 × Radne Raket 120 single cylinder, two-stroke, air-cooled aircraft engine with a 3.5:1 reduction drive, 10 kW (14 hp)
- Propellers: 2-bladed folding, 1.35 m (4 ft 5 in) diameter
See also
References
 |  |
