“Circa Reproductions Morane Saulnier N”的意思、由来-开放百科全书

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Circa Reproductions Morane Saulnier N

释义

Design and development
Specifications (Morane Saulnier N)
References
External links

name=Morane Saulnier N

image=

caption=

}}{{Infobox Aircraft Type

type=Amateur-built aircraft

national origin=Canada

manufacturer=Circa Reproductions

designer=Graham Lee

first flight=

introduced=

retired=

status=Plans available (2012)

primary user=

more users=

produced=

number built=

program cost=

unit cost= US$99 (plans only, 2015)

developed from= Morane-Saulnier N

variants with their own articles=
}}

The Circa Reproductions Morane Saulnier N, also called the Bullet, is a Canadian amateur-built aircraft that was designed by Graham Lee and produced by Circa Reproductions, of Surrey, British Columbia. The aircraft is supplied as plans for amateur construction.^[1]^[2]^[3]

The aircraft is a 90% scale replica of the First World War French Morane-Saulnier N fighter.^[1]

Design and development

The aircraft features a cable-braced mid-wing, a single-seat open cockpit, fixed conventional landing gear and a single engine in tractor configuration.^[1]^[3]

The aircraft is made from bolted-together aluminum tubing, with {{convert|1/8|in|mm|1|abbr=on}} plywood fuselage formers and stringers, with its flying surfaces covered in doped aircraft fabric. Its {{convert|23.9|ft|m|1|abbr=on}} span wing has an area of {{convert|117.5|sqft|m2|abbr=on}}. Standard engines recommended are the {{convert|50|hp|kW|0|abbr=on}} Rotax 503 and the {{convert|53|hp|kW|0|abbr=on}} Hirth 2704 two-stroke. The {{convert|60|hp|kW|0|abbr=on}} Volkswagen air-cooled engine four-stroke powerplant can be used, but the requirement for a smaller diameter propeller reduces performance.^[1]^[2]^[3]

Specifications (Morane Saulnier N)

{{Aircraft specs
|ref=Bayerl and Circa Reproductions^[1]^[2]
|prime units?=imp

|genhide=
|crew=one
|capacity=
|length m=
|length ft=19
|length in=3
|length note=
|span m=
|span ft=23
|span in=10
|span note=
|height m=
|height ft=6
|height in=
|height note=approximately
|wing area sqm=
|wing area sqft=117.5
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=
|empty weight lb=275
|empty weight note=
|gross weight kg=
|gross weight lb=600
|gross weight note=
|fuel capacity={{convert|12|u.s.gal}}
|more general=

|perfhide=
|max speed kmh=160
|max speed mph=
|max speed kts=
|max speed note=
|cruise speed kmh=115
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=48
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=115
|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=+5.7/-2.8
|roll rate=
|glide ratio=
|climb rate ms=3.25
|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=
|wing loading note=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}

References

1. ^¹²³⁴Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 97. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
2. ^¹²{{cite web|url = http://www.nieuports.com/index.asp?page=morane|title = The Morane Saulnier N or Bullet|accessdate = 29 September 2012|last = Circa Reproductions|date = n.d.}}
3. ^¹²Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 103. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}}

External links

{{Official website|http://nieuports.com/}}

2 : Homebuilt aircraft|Single-engined tractor aircraft

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