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词条 Skyfox Aviation Skyfox
释义

  1. Design and development

  2. Variants

  3. Specifications (CA-25)

  4. References

     Notes  Bibliography 

  5. External links

name=Skyfox image=24-3257 Skyfox CA25N Gazelle (8544393174).jpg caption=Skyfox CA25N Gazelle

}}{{Infobox Aircraft Type

type=Ultralight cabin monoplane national origin=Australia manufacturer=Skyfox Aviation designer= first flight=6 September 1989 introduced= retired= status= primary user= number built=100+ developed from= variants with their own articles=
}}

The Skyfox Aviation Skyfox is an Australian ultralight cabin monoplane designed by Skyfox Aviation of Queensland and first flown in 1989.[1] Originally sold as an ultralight it was later produced for general aviation use.[1]

Design and development

The Skyfox is a high-wing braced monoplane with a conventional tailwheel landing gear with a fixed tailwheel. It has a welded steel fuselage with fabric covering. The wings can be folded when not in use along the side of the fuselage.

Originally built to meet Australian ultralight regulations the latter CA-25 is built to JAR-VLA rules.[1]

Variants

CA-21

Volkswagen-engined variant, production ended in 1991

CA-22

Ultralight variant with a Rotax 912 engine.

CA-25 Impala

General aviation variant

CA-25N Gazelle

CA-25 with nosewheel landing gear.

Specifications (CA-25)

{{aerospecs
|ref=[1]
|met or eng?=eng
|crew=2
|capacity=
|length m=
|length ft=
|length in=
|span m=9.53
|span ft=31
|span in=3
|swept m=
|swept ft=
|swept in=
|rot number=
|rot dia m=
|rot dia ft=
|rot dia in=
|dia m=
|dia ft=
|dia in=
|width m=
|width ft=
|width in=
|height m=1.87
|height ft=6
|height in=1½
|wing area sqm=11.58
|wing area sqft=124.6
|swept area sqm=
|swept area sqft=
|rot area sqm=
|rot area sqft=
|volume m3=
|volume ft3=
|aspect ratio=
|empty weight kg=290
|empty weight lb=640
|gross weight kg=522
|gross weight lb=1150
|lift kg=
|lift lb=
|eng1 number=1
|eng1 type=Rotax 912 piston engine
|eng1 kw=58
|eng1 hp=78
|eng1 kn=
|eng1 lbf=
|eng1 kn-ab=
|eng1 lbf-ab=
|eng2 number=
|eng2 type=
|eng2 kw=
|eng2 hp=
|eng2 kn=
|eng2 lbf=
|eng2 kn-ab=
|eng2 lbf-ab=
|max speed kmh=176
|max speed mph=109
|max speed mach=
|cruise speed kmh=157
|cruise speed mph=98
|range km=598
|range miles=372
|endurance h=
|endurance min=
|ceiling m=
|ceiling ft=
|glide ratio=
|climb rate ms=2.44
|climb rate ftmin=800
|sink rate ms=
|sink rate ftmin=
|armament1=
|armament2=
|armament3=
|armament4=
|armament5=
|armament6=
}}{{aircontent
|see also=
|related=
|similar aircraft=
|lists=
}}

References

Notes

1. ^Taylor 1996, pp. 381-382

Bibliography

{{refbegin}}
  • {{cite book |last=Taylor |first= Michael J. H.|authorlink= |coauthors= |title= Brassey's World Aircraft & Systems Directory|year=1996 |publisher= Brassey's|location= London, England |isbn=1-85753-198-1|pages=}}
{{refend}}

External links

{{Commons category-inline}}{{Aero-1980s-stub}}

1 : Australian ultralight aircraft 1980–1989

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