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词条 Glasair GlaStar
释义

  1. Design and development

  2. Accidents and Incidents

  3. Variants

  4. Specifications (GlaStar)

  5. References

  6. External links

name=GlaStar image=File:Stoddard-hamilton.glastar.g-gery.arp.jpg caption=GlaStar

}}{{Infobox Aircraft Type

type=Amateur-built aircraft national origin=United States manufacturer=Stoddard-Hamilton Aircraft
Glasair Aviation
designer=Tom Hamilton first flight=1994 introduced= retired= status= Production completed circa 2005 primary user= more users= produced= number built=300 (2004)[1] program cost= unit cost= US$27,750 (2004 kit, less engine, paint, avionics, instruments, upholstery and propeller) developed from= variants with their own articles=Symphony SA-160
Glasair Sportsman 2+2
Plane Driven PD-1
}}

The Glasair GlaStar (sometimes Glastar) is an American amateur-built aircraft that was designed by Tom Hamilton and produced by Stoddard-Hamilton Aircraft and later Glasair Aviation. It was first flown in 1994 and was superseded in production by the Glasair Sportsman 2+2 c. 2005. When it was available the aircraft was supplied as a kit for amateur construction.[2][3][4]

Design and development

The GlaStar features a strut-braced high-wing, a two-seats-in-side-by-side configuration enclosed cockpit accessed via doors, fixed tricycle landing gear or conventional landing gear and a single engine in tractor configuration.[2][4]

The aircraft is made with a welded steel fuselage, with a fiberglass covering and aluminum wings. Its {{convert|35|ft|m|1|abbr=on}} span wing employs a NASA GA(W)-2 airfoil at the wing root, with a NASA GA(W)-2 mod at the wing tip. The wings have an area of {{convert|128|sqft|m2|abbr=on}}, mount flaps and can be folded for ground transportation or storage. The acceptable power range is {{convert|100|to|180|hp|kW|0|abbr=on}} and early engines used included the {{convert|100|hp|kW|0|abbr=on}} Rotax 912ULS. The aircraft proved underpowered with the Rotax, and later the {{convert|150|to|160|hp|kW|0|abbr=on}} Lycoming O-320 and the {{convert|180|hp|kW|0|abbr=on}} Lycoming O-360 four-stroke powerplants were used. The landing gear can be rapidly converted between tricycle and taildragger configurations. The cockpit is {{convert|44|in|cm|abbr=on}} wide and includes a large baggage area that will accommodate {{convert|200|lb|kg|abbr=on}} of cargo.[2][4][5]

Initial factory estimated construction time was 1200 hours.[3]

Accidents and Incidents

In 1996, a service recall was issued for the control yoke assembly of select GlaStar kits.{{Citation needed|date=October 2016}} In 1999, one of the GlaStar kits not included in the recall crashed, killing its two occupants.{{Citation needed|date=October 2016}}

Variants

//Symphony SA-160">Symphony SA-160

Type certified version, produced by Ostmecklenburgische Flugzeugbau (OMF) and later Symphony Aircraft.[2]

//Glasair Sportsman 2+2">Glasair Sportsman 2+2

Four seat development with a gross weight of {{convert|2350|lb|kg|0|abbr=on}} that replaced the original GlaStar in production.[6]

//Plane Driven PD-1">Plane Driven PD-1

Roadable version produced by Plane Driven.[7]

Specifications (GlaStar)

{{Aircraft specs
|ref=Bertrand and Kitplanes[2][3]
|prime units?=imp


|genhide=
|crew=one
|capacity=one passenger
|length m=
|length ft=22
|length in=0
|length note=
|span m=
|span ft=35
|span in=0
|span note=
|height m=
|height ft=7
|height in=0
|height note=
|wing area sqm=
|wing area sqft=128
|wing area note=
|aspect ratio=
|airfoil=Root: NASA GA(W)-2 airfoil, tip: NASA GA(W)-2 mod
|empty weight kg=
|empty weight lb=1200
|empty weight note=
|gross weight kg=
|gross weight lb=1960
|gross weight note=
|fuel capacity={{convert|50|u.s.gal}}
|more general=


|eng1 number=1
|eng1 name=Lycoming O-320
|eng1 type=four cylinder, air-cooled, four stroke aircraft engine
|eng1 kw=
|eng1 hp=160
|prop blade number=
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop note=


|perfhide=
|max speed kmh=
|max speed mph=170
|max speed kts=
|max speed note=
|cruise speed kmh=
|cruise speed mph=167
|cruise speed kts=
|cruise speed note=
|stall speed kmh=
|stall speed mph=45
|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=
|range nmi=1250
|range note=
|endurance=
|ceiling m=
|ceiling ft=20000
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=2075
|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=15.3
|wing loading note=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}

References

1. ^Downey, Julia: 2005 Kit Aircraft Directory, Kitplanes, Volume 21, Number 12, December 2004, page 60. Belvoir Publications. ISSN 0891-1851
2. ^Bertrand, Noel; Rene Coulon; et al: World Directory of Leisure Aviation 2003-04, page 183. Pagefast Ltd, Lancaster UK, 2003. ISSN 1368-485X
3. ^Downey, Julia: 1999 Kit Aircraft Directory, Kitplanes, Volume 15, Number 12, December 1998, page 68. Primedia Publications. ISSN 0891-1851
4. ^Purdy, Don: AeroCrafter - Homebuilt Aircraft Sourcebook, page 262. BAI Communications. {{ISBN|0-9636409-4-1}}
5. ^{{cite web|url = http://www.ae.illinois.edu/m-selig/ads/aircraft.html|title = The Incomplete Guide to Airfoil Usage |accessdate = 3 January 2012|last = Lednicer |first = David |authorlink = |year = 2010}}
6. ^Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 103. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
7. ^{{cite web|url=http://www.avweb.com/avwebflash/news/plane_driven_roadable_aircraft_oshkosh_airventure_trey_johnson_202922-1.html |title=Plane Driven's "Roadable" Glasair |publisher=Avweb.com |date=2010-07-23 |accessdate=2012-10-02}}

External links

{{Commons category-inline|Glasair GlaStar}}{{Glasair aircraft}}

5 : Homebuilt aircraft|Stoddard-Hamilton aircraft|Glasair aircraft|Single-engined tractor aircraft|High-wing aircraft

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