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词条 Dynamic Sport Rocket
释义

  1. Design and development

  2. Variants

  3. Specifications (Rocket 100)

  4. See also

  5. References

name=Rocket image= caption=

}}{{Infobox Aircraft Type

 type=Paramotor national origin=Poland manufacturer=Dynamic Sport designer= first flight= introduced= retired= status=Production completed primary user= more users= produced= number built= program cost= unit cost= €1,892 (2004) developed from= variants with their own articles=
}}

The Dynamic Sport Rocket is a series of Polish paramotors designed and produced by Dynamic Sport of Kielce for powered paragliding. Now out of production, when it was available the aircraft was supplied complete and ready-to-fly.[1]

Design and development

The Rocket 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 Radne Raket 120 {{convert|14|hp|kW|0|abbr=on}} engine in pusher configuration with a 3.25:1 ratio reduction drive and a {{convert|100|to|120|cm|in|0|abbr=on}} diameter propeller, depending on the model. The fuel tank capacity is {{convert|5|l}}, with {{convert|10|l}} optional.[1]

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.[1]

Variants

Rocket 100

Model with a Radne Raket 120 {{convert|14|hp|kW|0|abbr=on}} engine in pusher configuration with a 3.25:1 ratio reduction drive and a {{convert|100|cm|in|0|abbr=on}} diameter propeller. The fuel tank capacity is {{convert|5|l}}.[1]

Rocket 110

Model with a Radne Racket 120 {{convert|14|hp|kW|0|abbr=on}} engine in pusher configuration with a 3.25:1 ratio reduction drive and a {{convert|110|cm|in|0|abbr=on}} diameter propeller. The fuel tank capacity is {{convert|5|l}} or optionally {{convert|10|l}}.[1]

Rocket 115

Model with a Radne Racket 120 {{convert|14|hp|kW|0|abbr=on}} engine in pusher configuration with a 3.25:1 ratio reduction drive and a {{convert|115|cm|in|0|abbr=on}} diameter propeller. The fuel tank capacity is {{convert|5|l}} or optionally {{convert|10|l}}.[1]

Rocket 120

Model with a Radne Racket 120 {{convert|14|hp|kW|0|abbr=on}} engine in pusher configuration with a 3.25:1 ratio reduction drive and a {{convert|120|cm|in|0|abbr=on}} diameter propeller. The fuel tank capacity is {{convert|5|l}} or optionally {{convert|10|l}}.[1]

Specifications (Rocket 100)

{{Aircraft specs
|ref=Bertrand[1]
|prime units?=met


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|crew=one
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|empty weight kg=17
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|gross weight lb=
|gross weight note=
|fuel capacity={{convert|5|l}}
|more general=


|eng1 number=1
|eng1 name=Radne Raket 120
|eng1 type=single cylinder, two-stroke, air-cooled aircraft engine, with a 3.25:1 reduction drive
|eng1 kw=
|eng1 hp=
|prop blade number=2
|prop name=fixed pitch
|prop dia m=1.00
|prop dia ft=
|prop dia in=
|prop note=


|perfhide=Y
|max speed kmh=
|max speed mph=
|max speed kts=
|max speed note=
|cruise speed kmh=
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|range km=
|range miles=
|range nmi=
|range note=
|endurance=
|ceiling m=
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=
|climb rate note=
|time to altitude=
|sink rate ms=
|sink rate ftmin=
|sink rate note=
|lift to drag=
|wing loading kg/m2=
|wing loading lb/sqft=
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|power/mass=
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}}

See also

  • Dynamic Sport Climber

References

1. ^1 2 3 4 5 6 7 Bertrand, Noel; Rene Coulon; et al: World Directory of Leisure Aviation 2003-04, page 66. Pagefast Ltd, Lancaster UK, 2003. ISSN 1368-485X
{{Dynamic Sport aircraft}}

4 : Dynamic Sport aircraft|Polish ultralight aircraft 2000–2009|Single-engined pusher aircraft|Paramotors
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