Paramotor Mosquito
{{Short description|Polish paramotor}}
{{Use dmy dates|date=January 2022}}
{{Use American English|date=January 2022}}
| {{Infobox aircraft begin
| name= Mosquito | image= | caption= }}{{Infobox aircraft type | type=Paramotor | national origin=Poland | manufacturer=Paramotor Napedy Paralotniowe | designer=Ryszrd Zygadio | first flight= | introduced= | retired= | status=Production completed | primary user= | more users= | produced= | number built= | developed from= | variants with their own articles= }} |
The Paramotor Mosquito is a Polish paramotor that was designed by Ryszrd Zygadio and produced by Paramotor Napedy Paralotniowe ({{langx|en|Paragliding Paramotor Drives}}) of Warsaw for powered paragliding. Now out of production, when it was available the aircraft was supplied complete and ready-to-fly.Bertrand, Noel; Rene Coulon; et al: World Directory of Leisure Aviation 2003-04, page 72. Pagefast Ltd, Lancaster UK, 2003. ISSN 1368-485X
Design and development
The Mosquito was designed to comply with the US FAR 103 Ultralight Vehicles rules as well as European regulations. It features a paraglider-style wing, single-place accommodation and a single engine in pusher configuration with a reduction drive and a {{convert|100|to|125|cm|in|0|abbr=on}} diameter two-bladed composite propeller, all depending on the model. The aircraft is built from a combination of aluminium, with a stainless steel tube propeller cage.
As is the case with all paramotors, take-off and landing is accomplished by foot. Inflight steering is accomplished via handles that actuate the canopy brakes, creating roll and yaw.
Variants
;Mosquito M21Y
:Model with a {{convert|21|hp|kW|0|abbr=on}} Cors'Air M21Y engine in pusher configuration with a 2.5:1 ratio reduction drive and a {{convert|120|cm|in|0|abbr=on}} diameter two-bladed composite propeller. The fuel tank capacity is {{convert|9|L}}, with {{convert|15|L}} optional.
;Mosquito 120
:Model with a {{convert|14|hp|kW|0|abbr=on}} Radne Raket 120 engine in pusher configuration with a 3.6:1 ratio reduction drive and a {{convert|120|cm|in|0|abbr=on}} diameter two-bladed composite propeller. The fuel tank capacity is {{convert|5|L}}.
;Mosquito Radne 100
:Model with a {{convert|14|hp|kW|0|abbr=on}} Radne Raket 120 engine in pusher configuration with a 3.6:1 ratio reduction drive and a {{convert|120|cm|in|0|abbr=on}} diameter two-bladed composite propeller. The fuel tank capacity is {{convert|9|L}}.
;Mosquito Top
:Model with a {{convert|12|hp|kW|0|abbr=on}} Per Il Volo Top 80 engine in pusher configuration with a 4:1 ratio reduction drive and a {{convert|125|cm|in|0|abbr=on}} diameter two-bladed composite propeller. The fuel tank capacity is {{convert|9|L}}, with {{convert|11|L}} optional.
Specifications (Mosquito Top)
{{Aircraft specs
|prime units?=met
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|empty weight kg=23
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|fuel capacity={{convert|9|L}}, {{convert|11|L}} optional
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|eng1 number=1
|eng1 name=Per Il Volo Top 80
|eng1 type=single cylinder, two-stroke, air-cooled aircraft engine, with a X:1 reduction drive
|eng1 kw=
|eng1 hp=12
|prop blade number=2
|prop name=composite, fixed pitch
|prop dia m=1.25
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References
{{reflist}}
External links
- {{Official website|http://paramotor.home.pl/}}
Category:2000s Polish ultralight aircraft