“Amax Vixen 105”的意思、由来-开放百科全书

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Amax Vixen 105

释义

Design and development
Specifications (Vixen 105)
References

name= Vixen 105

image=

caption=

}}{{Infobox Aircraft Type

type=Homebuilt aircraft

national origin=Australia

manufacturer=Amax Engineering

designer=

first flight=

introduced=

retired=

status=Production completed

primary user=

more users=

produced=

number built=At least one

program cost=

unit cost= US$14,000 (kit, less engine, propeller and instruments, 1998)

developed from=

variants with their own articles=
}}

The Amax Vixen 105 is an Australian homebuilt aircraft that was designed and produced by Amax Engineering of Donvale, Victoria. When it was available the aircraft was supplied as a kit for amateur construction.^[1]

Design and development

The Vixen 105 features a strut-braced high-wing, a two-seats-in-side-by-side configuration enclosed cabin with doors, fixed tricycle landing gear or optionally conventional landing gear and a single engine in tractor configuration.^[1]

The aircraft is made from composites. Its {{convert|28.50|ft|m|1|abbr=on}} span wing has optional flaps and a wing area of {{convert|128.00|sqft|m2|abbr=on}}. The standard engine used is the {{convert|105|hp|kW|0|abbr=on}} Subaru EA81 automotive conversion powerplant.^[1]

Optional equipment when the kit was supplied by the factory included wing flaps, long range fuel tanks, wheel pants and sprung steel main landing gear.^[1]

The Vixen 105 has an empty weight of {{convert|500|lb|kg|abbr=on}} and a gross weight of {{convert|1200|lb|kg|abbr=on}}, giving a useful load of {{convert|700|lb|kg|abbr=on}}. With full fuel of {{convert|16|u.s.gal}} the payload is {{convert|604|lb|kg|abbr=on}}.^[1]

The manufacturer estimates the construction time from the supplied kit as 300 hours.^[1]

Specifications (Vixen 105)

{{Aircraft specs
|ref=AeroCrafter^[1]
|prime units?=imp

|genhide=
|crew=one
|capacity=one passenger
|length m=
|length ft=18.7
|length in=
|length note=
|span m=
|span ft=28
|span in=6
|span note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=
|wing area sqft=128.00
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=
|empty weight lb=500
|empty weight note=
|gross weight kg=
|gross weight lb=1200
|gross weight note=
|fuel capacity={{convert|16|u.s.gal}}
|more general=

|perfhide=
|max speed kmh=
|max speed mph=130
|max speed kts=
|max speed note=
|cruise speed kmh=
|cruise speed mph=100
|cruise speed kts=
|cruise speed note=
|stall speed kmh=
|stall speed mph=40
|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=350
|range nmi=
|range note=
|endurance=
|ceiling m=
|ceiling ft=14000
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=900
|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=9.4
|wing loading note=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}

References

1. ^¹²³⁴⁵⁶Purdy, Don: AeroCrafter - Homebuilt Aircraft Sourcebook, Fifth Edition, page 114. BAI Communications, 15 July 1998. {{ISBN|0-9636409-4-1}}

5 : Amax Engineering aircraft|Australian sport aircraft 1990–1999|Single-engined tractor aircraft|High-wing aircraft|Homebuilt aircraft

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