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Glasair GlaStar

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 It was first flown in 1994 and was superseded in production by the Glasair Sportsman 2+2 c. 2005.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]

GlaStar
GlaStar
Role Amateur-built aircraft
National origin United States
Manufacturer Stoddard-Hamilton Aircraft
Glasair Aviation
Designer Tom Hamilton
First flight 1994
Status Production completed circa 2005
Number built 300 (2004)[1]
Variants Symphony SA-160
Glasair Sportsman 2+2
Plane Driven PD-1

Design and development edit

 
GlaStar

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 35 ft (10.7 m) 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 128 sq ft (11.9 m2), mount flaps and can be folded for ground transportation or storage. The acceptable power range is 100 to 180 hp (75 to 134 kW) and early engines used included the 100 hp (75 kW) Rotax 912ULS. The aircraft proved underpowered with the Rotax, and later the 150 to 160 hp (112 to 119 kW) Lycoming O-320 and the 180 hp (134 kW) Lycoming O-360 four-stroke powerplants were used. The landing gear can be rapidly converted between tricycle and taildragger configurations. The cockpit is 44 in (110 cm) wide and includes a large baggage area that will accommodate 200 lb (91 kg) of cargo.[2][4][5]

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

Accidents and Incidents edit

In 1996, a service recall was issued for the control yoke assembly of select GlaStar kits.[6] In 1999, one of the GlaStar kits not included in the recall crashed, killing its two occupants.[7]

Variants edit

 
Symphony SA-160
 
Glasair Sportsman 2+2
 
Plane Driven PD-1
Symphony SA-160
Type certified version, produced by Ostmecklenburgische Flugzeugbau (OMF) and later Symphony Aircraft.[2]
Glasair Sportsman 2+2
Four seat development with a gross weight of 2,350 lb (1,066 kg) that replaced the original GlaStar in production.[8]
Plane Driven PD-1
Roadable version produced by Plane Driven.[9]

Specifications (GlaStar) edit

Data from Bertrand and Kitplanes[2][3]

General characteristics

  • Crew: one
  • Capacity: one passenger
  • Length: 22 ft 0 in (6.71 m)
  • Wingspan: 35 ft 0 in (10.67 m)
  • Height: 7 ft 0 in (2.13 m)
  • Wing area: 128 sq ft (11.9 m2)
  • Airfoil: Root: NASA GA(W)-2 airfoil, tip: NASA GA(W)-2 mod
  • Empty weight: 1,200 lb (544 kg)
  • Gross weight: 1,960 lb (889 kg)
  • Fuel capacity: 50 U.S. gallons (190 L; 42 imp gal)
  • Powerplant: 1 × Lycoming O-320 four cylinder, air-cooled, four stroke aircraft engine, 160 hp (120 kW)

Performance

  • Maximum speed: 170 mph (270 km/h, 150 kn)
  • Cruise speed: 167 mph (269 km/h, 145 kn)
  • Stall speed: 45 mph (72 km/h, 39 kn)
  • Range: 1,440 mi (2,320 km, 1,250 nmi)
  • Service ceiling: 20,000 ft (6,100 m)
  • Rate of climb: 2,075 ft/min (10.54 m/s)
  • Wing loading: 15.3 lb/sq ft (75 kg/m2)

References edit

  1. ^ Downey, Julia: 2005 Kit Aircraft Directory, Kitplanes, Volume 21, Number 12, December 2004, page 60. Belvoir Publications. ISSN 0891-1851
  2. ^ a b c d e Bertrand, Noel; Rene Coulon; et al: World Directory of Leisure Aviation 2003-04, page 183. Pagefast Ltd, Lancaster UK, 2003. ISSN 1368-485X
  3. ^ a b c Downey, Julia: 1999 Kit Aircraft Directory, Kitplanes, Volume 15, Number 12, December 1998, page 68. Primedia Publications. ISSN 0891-1851
  4. ^ a b c Purdy, Don: AeroCrafter - Homebuilt Aircraft Sourcebook, page 262. BAI Communications. ISBN 0-9636409-4-1
  5. ^ Lednicer, David (2010). . Archived from the original on April 20, 2010. Retrieved January 3, 2012.
  6. ^ "Glasair". Glasair Aviation.
  7. ^ "Glastar crash". William Jerry (Champ) Champion.
  8. ^ Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 103. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
  9. ^ "Plane Driven's "Roadable" Glasair". Avweb.com. July 23, 2010. Retrieved October 2, 2012.

External links edit

  Media related to Glasair GlaStar at Wikimedia Commons

glasair, glastar, sometimes, glastar, american, amateur, built, aircraft, that, designed, hamilton, produced, stoddard, hamilton, aircraft, later, glasair, aviation, first, flown, 1994, superseded, production, glasair, sportsman, 2005, when, available, aircraf. 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 GlaStar GlaStar Role Amateur built aircraft National origin United States Manufacturer Stoddard Hamilton AircraftGlasair Aviation Designer Tom Hamilton First flight 1994 Status Production completed circa 2005 Number built 300 2004 1 Variants Symphony SA 160Glasair Sportsman 2 2Plane Driven PD 1 Contents 1 Design and development 2 Accidents and Incidents 3 Variants 4 Specifications GlaStar 5 References 6 External linksDesign and development edit nbsp GlaStar 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 35 ft 10 7 m 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 128 sq ft 11 9 m2 mount flaps and can be folded for ground transportation or storage The acceptable power range is 100 to 180 hp 75 to 134 kW and early engines used included the 100 hp 75 kW Rotax 912ULS The aircraft proved underpowered with the Rotax and later the 150 to 160 hp 112 to 119 kW Lycoming O 320 and the 180 hp 134 kW Lycoming O 360 four stroke powerplants were used The landing gear can be rapidly converted between tricycle and taildragger configurations The cockpit is 44 in 110 cm wide and includes a large baggage area that will accommodate 200 lb 91 kg of cargo 2 4 5 Initial factory estimated construction time was 1200 hours 3 Accidents and Incidents editIn 1996 a service recall was issued for the control yoke assembly of select GlaStar kits 6 In 1999 one of the GlaStar kits not included in the recall crashed killing its two occupants 7 Variants edit nbsp Symphony SA 160 nbsp Glasair Sportsman 2 2 nbsp Plane Driven PD 1 Symphony SA 160 Type certified version produced by Ostmecklenburgische Flugzeugbau OMF and later Symphony Aircraft 2 Glasair Sportsman 2 2 Four seat development with a gross weight of 2 350 lb 1 066 kg that replaced the original GlaStar in production 8 Plane Driven PD 1 Roadable version produced by Plane Driven 9 Specifications GlaStar editData from Bertrand and Kitplanes 2 3 General characteristicsCrew one Capacity one passenger Length 22 ft 0 in 6 71 m Wingspan 35 ft 0 in 10 67 m Height 7 ft 0 in 2 13 m Wing area 128 sq ft 11 9 m2 Airfoil Root NASA GA W 2 airfoil tip NASA GA W 2 mod Empty weight 1 200 lb 544 kg Gross weight 1 960 lb 889 kg Fuel capacity 50 U S gallons 190 L 42 imp gal Powerplant 1 Lycoming O 320 four cylinder air cooled four stroke aircraft engine 160 hp 120 kW Performance Maximum speed 170 mph 270 km h 150 kn Cruise speed 167 mph 269 km h 145 kn Stall speed 45 mph 72 km h 39 kn Range 1 440 mi 2 320 km 1 250 nmi Service ceiling 20 000 ft 6 100 m Rate of climb 2 075 ft min 10 54 m s Wing loading 15 3 lb sq ft 75 kg m2 References edit Downey Julia 2005 Kit Aircraft Directory Kitplanes Volume 21 Number 12 December 2004 page 60 Belvoir Publications ISSN 0891 1851 a b c d e Bertrand Noel Rene Coulon et al World Directory of Leisure Aviation 2003 04 page 183 Pagefast Ltd Lancaster UK 2003 ISSN 1368 485X a b c Downey Julia 1999 Kit Aircraft Directory Kitplanes Volume 15 Number 12 December 1998 page 68 Primedia Publications ISSN 0891 1851 a b c Purdy Don AeroCrafter Homebuilt Aircraft Sourcebook page 262 BAI Communications ISBN 0 9636409 4 1 Lednicer David 2010 The Incomplete Guide to Airfoil Usage Archived from the original on April 20 2010 Retrieved January 3 2012 Glasair Glasair Aviation Glastar crash William Jerry Champ Champion Bayerl Robby Martin Berkemeier et al World Directory of Leisure Aviation 2011 12 page 103 WDLA UK Lancaster UK 2011 ISSN 1368 485X Plane Driven s Roadable Glasair Avweb com July 23 2010 Retrieved October 2 2012 External links edit nbsp Media related to Glasair GlaStar at Wikimedia Commons Retrieved from https en wikipedia org w index php title Glasair GlaStar amp oldid 1177436999, wikipedia, wiki, book, books, library,

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