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词条 Rogers Sportaire
释义

  1. Design and development

  2. Operational history

  3. Specifications (Sportaire)

  4. References

  5. External links

name=Sportaire image= caption=

}}{{Infobox Aircraft Type

type=Homebuilt aircraft national origin=United States manufacturer=Rogers Aircraft designer=David M. Rogers first flight= introduced= retired= status= Production completed (1959) primary user= more users= produced= 1959 number built=One program cost= unit cost= developed from= variants with their own articles=
}}

The Rogers Sportaire is an American homebuilt aircraft that was designed David M. Rogers and produced by Rogers Aircraft of Riverside, California, introduced in 1959. The aircraft was supplied in the form of plans for amateur construction, but plans are no longer available. Only one was built.[1][2]

Design and development

The aircraft features a cantilever low-wing, a two-seats-in-side-by-side configuration enclosed cockpit under a bubble canopy, fixed tricycle landing gear and a single engine in tractor configuration.[1]

The aircraft fuselage is made from welded steel tubing, with the {{convert|26.3|ft|m|1|abbr=on}} span wing made from wood, all covered in doped aircraft fabric. The engine used in the sole example is a {{convert|125|hp|kW|0|abbr=on}} Lycoming O-290 powerplant.[1][2]

The aircraft has an empty weight of {{convert|984|lb|kg|abbr=on}} and a gross weight of {{convert|1600|lb|kg|abbr=on}}, giving a useful load of {{convert|616|lb|kg|abbr=on}}. With full fuel of {{convert|22|u.s.gal}} the payload is {{convert|484|lb|kg|abbr=on}}.[1]

Operational history

By October 2013 only one example had been registered in the United States with the Federal Aviation Administration.[2]

Specifications (Sportaire)

{{Aircraft specs
|ref=Plane and Pilot[1]
|prime units?=imp


|genhide=
|crew=one
|capacity=one passenger
|length m=
|length ft=18
|length in=0
|length note=
|span m=
|span ft=26
|span in=4
|span note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=
|wing area sqft=
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=
|empty weight lb=984
|empty weight note=
|gross weight kg=
|gross weight lb=1600
|gross weight note=
|fuel capacity={{convert|22|u.s.gal}}
|more general=


|eng1 number=1
|eng1 name=Lycoming O-290
|eng1 type=four cylinder, air-cooled, four stroke aircraft engine
|eng1 kw=
|eng1 hp=125
|prop blade number=
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop note=


|perfhide=
|max speed kmh=
|max speed mph=160
|max speed kts=
|max speed note=
|cruise speed kmh=
|cruise speed mph=150
|cruise speed kts=
|cruise speed note=
|stall speed kmh=
|stall speed mph=55
|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=400
|range nmi=
|range note=
|endurance=
|ceiling m=
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=1000
|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=
|wing loading note=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}

References

1. ^Plane and Pilot: 1978 Aircraft Directory, page 154. Werner & Werner Corp, Santa Monica CA, 1977. {{ISBN|0-918312-00-0}}
2. ^{{cite web|url = http://registry.faa.gov/aircraftinquiry/NNum_Results.aspx?NNumbertxt=311DR|title = N-Number Inquiry Results - N311DR|accessdate = 22 October 2013|last = Federal Aviation Administration|date = 22 October 2013}}

External links

  • Photo of the Sportaire airframe under restoration
  • Photo of the Sportaire instrument panel under restoration
  • Photo of the Sportaire dataplate

5 : Rogers Aircraft|United States sport aircraft 1950–1959|Single-engined tractor aircraft|Low-wing aircraft|Homebuilt aircraft

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