“CSA PS-38 Tourer”的意思、由来-开放百科全书

The CSA PS-38 Tourer is a Czech light-sport aircraft under development by Czech Sport Aircraft of Prague, introduced at the AERO Friedrichshafen show in 2014. The aircraft is intended to be supplied complete and ready-to-fly.^[1]

Design and development

The PS-38 Tourer was designed for private use for cross-country flying as well as the law enforcement role.^[1]

The aircraft was designed to comply with the US light-sport aircraft rules. It features a cantilever high-wing, an enclosed cabin with two-seats-in-side-by-side configuration accessed by doors, fixed tricycle landing gear and a single engine in tractor configuration.^[1]

The aircraft is made with an aluminum semi-monocoque structure. Its {{convert|8.6|m|ft|1|abbr=on}} span forward-swept wing has an area of {{convert|12.3|m2|sqft|abbr=on}} and mounts flaps. The standard engine used is the {{convert|100|hp|kW|0|abbr=on}} Rotax 912ULS four-stroke powerplant. The forward-swept wing provides improved visibility to the pilot in turns.^[1]

As of January 2018, the design does not appear on the Federal Aviation Administration's list of approved special light-sport aircraft.^[2]

The design also did not appear on the manufacturer's website as offered for sale in February 2017.^[3]

Specifications (PS-38 Tourer)

|genhide=
|crew=one
|capacity=one passenger
|length m=
|length ft=
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|length note=
|span m=8.6
|span ft=
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|height m=
|height ft=
|height in=
|height note=
|wing area sqm=12.3
|wing area sqft=
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=381
|empty weight lb=
|empty weight note=
|gross weight kg=600
|gross weight lb=
|gross weight note=
|fuel capacity={{convert|114|l}} in two tanks
|more general=

|perfhide=
|max speed kmh=220
|max speed mph=
|max speed kts=
|max speed note=
|cruise speed kmh=172
|cruise speed mph=
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|cruise speed note=
|stall speed kmh=55
|stall speed mph=
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|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|range km=
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|ceiling m=
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|ceiling note=
|g limits=
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|climb rate ms=
|climb rate ftmin=
|climb rate note=
|time to altitude=
|sink rate ms=
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|lift to drag=
|wing loading kg/m2=48.8
|wing loading lb/sqft=
|wing loading note=
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References

1. ^¹²³⁴Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 42. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}}
2. ^{{cite web|url = https://www.faa.gov/aircraft/gen_av/light_sport/media/SLSA_Directory.xlsx|title = SLSA Make/Model Directory|accessdate = 29 January 2018|last = Federal Aviation Administration|date = 11 January 2018}}
3. ^{{cite web|url = http://www.czechsportaircraft.com/aircraft/|title = Aircraft|accessdate = 5 February 2017|author = Czech Sport Aircraft|year = 2017}}

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