Английская Википедия:DTA J-RO

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Шаблон:Short description Шаблон:Use dmy dates Шаблон:Use British English

The DTA J-RO (Шаблон:Trans) is a French autogyro designed and produced by DTA sarl of Montélimar. The aircraft is supplied complete and ready-to-fly.[1]

Design and development

The J-RO was designed to combine the advantages of an ultralight trike with an autogyro. As such it is a "Cabriolet" (convertible) design whereby the gull-winged doors are removable to allow open air flight in the summertime and an enclosed cockpit for cooler weather. The doors are a factory option and may be purchased and installed later.[1]

The design features a single main rotor, a two-seats-in side-by-side configuration enclosed or open cockpit with a windshield, tricycle landing gear with wheel pants and a four-cylinder, liquid and air-cooled, four stroke Шаблон:Convert Rotax 912ULS or turbocharged Шаблон:Convert Rotax 914 engine in pusher configuration. It has a Kevlar belt-driven pre-rotator for the main rotor.[1][2]

The aircraft fuselage is made from carbon fiber reinforced polymer. Its two-bladed rotor has a diameter of Шаблон:Convert and a chord of Шаблон:Convert. The aircraft has a typical empty weight of Шаблон:Convert and a gross weight of Шаблон:Convert, giving a useful load of Шаблон:Convert. With full fuel of Шаблон:Convert the payload for the pilot, passenger and baggage is Шаблон:Convert.[1]

In noise testing for acceptance in Switzerland the design produced 62.4 dB. The Swiss testing requires the design produce no more than a maximum of 65 dB for this class of aircraft.[2]

Specifications (J-RO)

Шаблон:Aircraft specs

See also

References

Шаблон:Reflist

External links

Шаблон:Commons category

Шаблон:DTA aircraft

  1. 1,0 1,1 1,2 1,3 Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 192. Flying Pages Europe SARL, 2015. Шаблон:ISSN
  2. 2,0 2,1 Шаблон:Cite web