172:
Model with a Radne Racket 120 14 hp (10 kW) engine in pusher configuration with a 3.25:1 ratio reduction drive and a 120 cm (47 in) diameter propeller. The fuel tank capacity is 5 litres (1.1 imp gal; 1.3 US gal) or optionally 10 litres (2.2 imp gal;
165:
Model with a Radne Racket 120 14 hp (10 kW) engine in pusher configuration with a 3.25:1 ratio reduction drive and a 115 cm (45 in) diameter propeller. The fuel tank capacity is 5 litres (1.1 imp gal; 1.3 US gal) or optionally 10 litres (2.2 imp gal;
158:
Model with a Radne Racket 120 14 hp (10 kW) engine in pusher configuration with a 3.25:1 ratio reduction drive and a 110 cm (43 in) diameter propeller. The fuel tank capacity is 5 litres (1.1 imp gal; 1.3 US gal) or optionally 10 litres (2.2 imp gal;
124:
and a 100 to 120 cm (39 to 47 in) diameter propeller, depending on the model. The fuel tank capacity is 5 litres (1.1 imp gal; 1.3 US gal), with 10 litres (2.2 imp gal; 2.6 US gal) optional.
128:
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.
350:
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and a 100 cm (39 in) diameter propeller. The fuel tank capacity is 5 litres (1.1 imp gal; 1.3 US gal).
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105:
96:. Now out of production, when it was available the aircraft was supplied complete and ready-to-fly.
378:
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145:
117:
8:
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93:
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2-bladed fixed pitch, 1.00 m (3 ft 3 in) diameter
89:
78:
47:
286:, page 66. Pagefast Ltd, Lancaster UK, 2003. ISSN 1368-485X
211:
5 litres (1.1 imp gal; 1.3 US gal)
112:-style wing, single-place accommodation and a single
108:
rules as well as
European regulations. It features a
396:
177:
104:The Rocket was designed to comply with the US
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284:World Directory of Leisure Aviation 2003-04
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282:Bertrand, Noel; Rene Coulon; et al:
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144:14 hp (10 kW) engine in
116:14 hp (10 kW) engine in
14:
431:
410:2000s Polish ultralight aircraft
415:Single-engined pusher aircraft
1:
254:
7:
242:
178:Specifications (Rocket 100)
131:
106:FAR 103 Ultralight Vehicles
10:
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369:
331:
84:designed and produced by
23:
205:17 kg (37 lb)
190:General characteristics
405:Dynamic Sport aircraft
173:2.6 US gal).
166:2.6 US gal).
159:2.6 US gal).
100:Design and development
249:Dynamic Sport Climber
67:Production completed
148:with a 3.25:1 ratio
146:pusher configuration
120:with a 3.25:1 ratio
118:pusher configuration
75:Dynamic Sport Rocket
94:powered paragliding
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221:single cylinder,
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229:, with a 3.25:1
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36:Type of aircraft
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16:Polish Paramotor
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231:reduction drive
227:aircraft engine
219:Radne Raket 120
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150:reduction drive
142:Radne Raket 120
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122:reduction drive
114:Radne Raket 120
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77:is a series of
43:National origin
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209:Fuel capacity:
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324:Dynamic Sport
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225:, air-cooled
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203:Empty weight:
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140:Model with a
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86:Dynamic Sport
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54:Manufacturer
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333:Paragliders
236:Propellers:
215:Powerplant:
420:Paramotors
399:Categories
371:Paramotors
255:References
223:two-stroke
169:Rocket 120
162:Rocket 115
155:Rocket 110
137:Rocket 100
110:paraglider
82:paramotors
183:Data from
33:Paramotor
326:aircraft
243:See also
185:Bertrand
132:Variants
379:Climber
64:Status
24:Rocket
384:Rocket
351:Magnum
346:Gravis
341:Enigma
90:Kielce
79:Polish
48:Poland
361:Viper
356:Raven
197:Crew:
29:Role
217:1 ×
92:for
73:The
199:one
88:of
401::
263:^
316:e
309:t
302:v
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