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词条 St Croix Excelsior
释义

  1. Design and development

  2. Specifications (Excelsior)

  3. References

  4. External links

name=Excelsior image= caption=

}}{{Infobox Aircraft Type

type=Ultralight aircraft national origin=United States manufacturer=St Croix Aircraft designer=Chad Wille and Charles Wille first flight=1980 introduced= retired= status=Production completed primary user= more users= produced= 1980-circa 2000 number built= program cost= unit cost= US$79.00 (plans only, 1998 price)[1] developed from= variants with their own articles=
}}

The St Croix Excelsior ({{lang-en|ever higher}}) is an American ultralight aircraft that was designed by Chad Wille and Charles Wille, produced by St Croix Aircraft of Corning, Iowa and first flown in 1980. The aircraft was supplied in the form of plans for amateur construction with some hard-to-make parts available as well as partial kits.[1][2][3][4]

Design and development

The Excelsior was designed to comply with the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of {{convert|254|lb|kg|0|abbr=on}}. The aircraft has a standard empty weight of {{convert|250|lb|kg|0|abbr=on}}. It features a strut-braced high-wing, a single-seat, open cockpit, tricycle landing gear and a single engine in pusher configuration.[2]

The aircraft fuselage is made from welded 4130 steel tubing, with the wings and tail built from riveted sheet aluminum, aluminum tubing and covered with doped aircraft fabric covering. Its straight leading edge, tapered trailing edge, {{convert|34.6|ft|m|1|abbr=on}} span wing is braced with a single lift strut per side. The pilot sits in an open cockpit, with a small windshield. The engine and tail configuration are unconventional. The specified Zenoah G25 {{convert|20|hp|kW|0|abbr=on}} engine is mounted on top of the high wing and drives the tail-mounted propeller through a flexible extension shaft, that is designed to eliminate vibrations. The tailplane and elevator are mounted on top of the rear fuselage, with the fin and rudder mounted below the tailplane, providing protection for the propeller from contacting the ground. The controls are conventional, except that roll control is provided by spoilers, rather than ailerons. The landing gear consists of suspended main gear, a nose wheel and a rudder-mounted rear skid.[1][2]

The aircraft has enough gliding performance to be soared. The construction time from the plans is estimated at 400 hours. Plans were intermittently available between 1980 and about 2000, but from 2001 the design was not advertised as being available by the company any longer.[2][3][5]

Specifications (Excelsior)

{{Aircraft specs
|ref=Cliche, Kitplanes and Purdy[1][2][4]
|prime units?=imp


|genhide=
|crew=one
|capacity=
|length m=
|length ft=16
|length in=6
|length note=
|span m=
|span ft=34
|span in=7
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|height m=
|height ft=6
|height in=0
|height note=
|wing area sqm=
|wing area sqft=136
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=
|empty weight lb=250
|empty weight note=
|gross weight kg=
|gross weight lb=525
|gross weight note=
|fuel capacity={{convert|5|u.s.gal}}
|more general=


|eng1 number=1
|eng1 name=Zenoah G25
|eng1 type=
|eng1 kw=
|eng1 hp=20
|prop blade number=
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop note=


|perfhide=
|max speed kmh=
|max speed mph=75
|max speed kts=
|max speed note=
|cruise speed kmh=
|cruise speed mph=65
|cruise speed kts=
|cruise speed note=
|stall speed kmh=
|stall speed mph=25
|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=125
|range nmi=
|range note=
|endurance=
|ceiling m=
|ceiling ft=
|ceiling note=
|g limits=+4/-4
|roll rate=
|glide ratio=20:1
|climb rate ms=
|climb rate ftmin=600
|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=
}}{{aircontent
|see also=
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|similar aircraft=
|lists=
}}

References

1. ^Purdy, Don: AeroCrafter - Homebuilt Aircraft Sourcebook, page 247. BAI Communications. {{ISBN|0-9636409-4-1}}
2. ^Cliche, Andre: Ultralight Aircraft Shopper's Guide 8th Edition, page E-15. Cybair Limited Publishing, 2001. {{ISBN|0-9680628-1-4}}
3. ^{{Cite web|url = http://virtualultralightmuseum.com/e.htm#excelsior|title = Excelsior|accessdate = 10 November 2011|last = Virtual Ultralight Museum|date = n.d.}}
4. ^Downey, Julia: 1999 Plans Aircraft Directory, Kitplanes, Volume 16, Number 1, January 1999, page 67. Primedia Publications. ISSN 0891-1851
5. ^Downey, Julia: 2001 Plans Aircraft Directory, Kitplanes, Volume 18, Number 1, January 2001, page 28. Kitplanes Acquisition Company. ISSN 0891-1851

External links

  • Photo of an Excelsior
{{St Croix aircraft}}

4 : St Croix aircraft|United States ultralight aircraft 1980–1989|Homebuilt aircraft|Single-engined pusher aircraft

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