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词条 Redback Buzzard
释义

  1. Design and development

  2. Specifications (version)

  3. References

  4. External links

name=Buzzard image= caption=

}}{{Infobox Aircraft Type

type=Helicopter national origin=Australia manufacturer=Redback Aviation designer= first flight= introduced= retired= status=Production completed (2013) primary user= more users= produced= number built=one program cost= unit cost= developed from= Star Aviation LoneStar variants with their own articles=
}}

The Redback Buzzard is an Australian helicopter that was designed and produced by Redback Aviation of Hoppers Crossing, Victoria. The aircraft was intended to be supplied as a kit for amateur construction, but only one prototype was ever completed and development ended.[1][2]

Design and development

The Buzzard was based on the second generation Star Aviation LoneStar helicopter to which Redback own the rights. The Buzzard was designed to be a minimalist helicopter, using a maximum of off-the-shelf parts and to comply with the homebuilt aircraft rules. It features a single main rotor, a single-seat open cockpit without a windshield, skid-type landing gear and a Suzuki {{convert|75|hp|kW|0|abbr=on}} four stroke engine.[1][2]

The aircraft fuselage is made from bolted-together aluminum tubing, with the tailboom built from carbon fibre. Its {{convert|6.10|m|ft|1|abbr=on}} diameter two-bladed rotor has a chord of {{convert|20|cm|in|1|abbr=on}}, with anti-torque handled by a conventional two-bladed tail rotor. The main rotor transmission uses a combination of V-belts and toothed belts. Pitch link controls are mounted inside the hollow rotor mast tube. The aircraft has an empty weight of {{convert|193|kg|lb|0|abbr=on}} and a gross weight of {{convert|386|kg|lb|0|abbr=on}}, giving a useful load of {{convert|193|kg|lb|0|abbr=on}}. With full fuel of {{convert|58.8|l}} the payload is {{convert|151|kg|lb|0|abbr=on}}.[1]

The company indicates that only one prototype was built and that it was sold, ending development of the aircraft, in favour of a new design, the Redback Aviation Spider.[2]

Specifications (version)

{{Aircraft specs
|ref=Bayerl[1]
|prime units?=met


|genhide=
|crew=one
|capacity=
|length m=
|length ft=
|length in=
|length note=
|width m=
|width ft=
|width in=
|width note=
|height m=
|height ft=
|height in=
|height note=
|airfoil=
|empty weight kg=192
|empty weight lb=
|empty weight note=
|gross weight kg=386
|gross weight lb=
|gross weight note=
|fuel capacity={{convert|58.5|l}}
|more general=


|eng1 number=1
|eng1 name=Suzuki
|eng1 type=four stroke automotive engine
|eng1 kw=
|eng1 hp=75
|rot number=1
|rot dia m=6.10
|rot dia ft=
|rot dia in=
|rot area sqm=
|rot area sqft=
|rot area note=


|perfhide=
|max speed kmh=169
|max speed mph=
|max speed kts=
|max speed note=
|cruise speed kmh=145
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|never exceed speed kmh=
|never exceed speed mph=
|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=
|roll rate=
|glide ratio=
|climb rate ms=5.0
|climb rate ftmin=
|climb rate note=
|time to altitude=
|disk loading kg/m2=
|disk loading lb/sqft=
|disk loading note=
|fuel consumption kg/km=
|fuel consumption lb/mi=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}

References

1. ^Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 193. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
2. ^{{cite web|url = http://www.redbackaviation.com/|title = Welcome To Redback Aviation's World Of Homebuilt Helicopters|accessdate = 7 February 2013|last = Redback Aviation|date = n.d.}}

External links

  • {{Official website|http://www.redbackaviation.com/}}
{{Redback aircraft}}

5 : Australian sport aircraft 2000–2009|Australian helicopters 2000–2009|Homebuilt aircraft|Single-engined piston helicopters|Redback Aviation aircraft

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