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engine in pusher configuration with a 4:1 ratio reduction drive and a 125 cm (49 in) diameter two-bladed composite propeller. The fuel tank capacity is 9 litres (2.0 imp gal; 2.4 US gal), with 11 litres (2.4 imp gal; 2.9 US gal)
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engine in pusher configuration with a 3.6:1 ratio reduction drive and a 120 cm (47 in) diameter two-bladed composite propeller. The fuel tank capacity is 9 litres (2.0 imp gal; 2.4 US gal).
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engine in pusher configuration with a 3.6:1 ratio reduction drive and a 120 cm (47 in) diameter two-bladed composite propeller. The fuel tank capacity is 5 litres (1.1 imp gal; 1.3 US gal).
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and a 120 cm (47 in) diameter two-bladed composite propeller. The fuel tank capacity is 9 litres (2.0 imp gal; 2.4 US gal), with 15 litres (3.3 imp gal; 4.0 US gal)
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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.
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and a 100 to 125 cm (39 to 49 in) diameter two-bladed composite propeller, all depending on the model. The aircraft is built from a combination of
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9 litres (2.0 imp gal; 2.4 US gal), 11 litres (2.4 imp gal; 2.9 US gal) optional
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105:. Now out of production, when it was available the aircraft was supplied complete and ready-to-fly.
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2-bladed composite, fixed pitch, 1.25 m (4 ft 1 in) diameter
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121:-style wing, single-place accommodation and a single engine in
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298:, page 72. Pagefast Ltd, Lancaster UK, 2003. ISSN 1368-485X
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rules as well as
European regulations. It features a
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that was designed by Ryszrd
Zygadio and produced by
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113:The Mosquito was designed to comply with the US
296:World Directory of Leisure Aviation 2003-04
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331:Paramotor Napedy Paralotniowe aircraft
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181:Model with a 14 hp (10 kW)
171:Model with a 14 hp (10 kW)
152:Model with a 21 hp (16 kW)
294:Bertrand, Noel; Rene Coulon; et al:
191:Model with a 12 hp (9 kW)
13:
14:
357:
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336:2000s Polish ultralight aircraft
341:Single-engined pusher aircraft
1:
266:
201:Specifications (Mosquito Top)
91:Paramotor Napedy Paralotniowe
58:Paramotor Napedy Paralotniowe
95:Paragliding Paramotor Drives
7:
143:
115:FAR 103 Ultralight Vehicles
10:
362:
256:, 8.9 kW (12 hp)
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23:
228:23 kg (51 lb)
213:General characteristics
109:Design and development
137:tube propeller cage.
75:Production completed
158:pusher configuration
123:pusher configuration
160:with a 2.5:1 ratio
103:powered paragliding
242:Per Il Volo Top 80
193:Per Il Volo Top 80
178:Mosquito Radne 100
83:Paramotor Mosquito
244:single cylinder,
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314:Official website
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36:Type of aircraft
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16:Polish paramotor
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254:reduction drive
250:aircraft engine
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183:Radne Raket 120
173:Radne Raket 120
162:reduction drive
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135:stainless steel
127:reduction drive
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67:Ryszrd Zygadio
43:National origin
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306:External links
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232:Fuel capacity:
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252:, with a X:1
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154:Cors'Air M21Y
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149:Mosquito M21Y
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188:Mosquito Top
168:Mosquito 120
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85:is a Polish
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260:Propellers:
238:Powerplant:
346:Paramotors
325:Categories
267:References
246:two-stroke
156:engine in
119:paraglider
93:(English:
206:Data from
196:optional.
165:optional.
133:, with a
131:aluminium
87:paramotor
64:Designer
33:Paramotor
24:Mosquito
208:Bertrand
144:Variants
125:with a
72:Status
99:Warsaw
48:Poland
220:Crew:
97:) of
29:Role
240:1 ×
101:for
81:The
222:one
327::
275:^
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