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Celair GA-1 Celstar

The Celair GA-1 Celstar is a South African mid-wing, single-seat, aerobatic glider that was designed by Pieter Celliers and produced by his company, Celair (Pty) Limited.[1]

GA-1 Celstar
Role Glider
National origin South Africa
Manufacturer Celair (Pty) Limited
Designer Pieter Celliers
First flight 1989
Status Production completed
Number built At least eight

Design and development edit

The GA-1 was especially intended for flying competitive glider aerobatics and the resulting airframe was designed to Joint Aviation Requirements 22 standards and stressed to 10 g.[1]

The aircraft is made from a combination of fibreglass and aramid. Its 11.2 m (36.7 ft) span wing employs a Wortmann FX-71-L-150/25 airfoil. The ailerons are full-span and mass-balanced. Dive brakes are used for approach control.[1][2]

At least eight were produced, with two exported to Switzerland and six to the United States.[3]

Operational history edit

In August 2011 there were two GA-1s registered in the US with the Federal Aviation Administration. US-registered aircraft are in the Experimental - Racing/Exhibition category.[4]

Specifications (GA-1) edit

Data from Sailplane Directory[1]

General characteristics

  • Crew: one
  • Wingspan: 11.2 m (36 ft 9 in)
  • Wing area: 11.54 m2 (124.2 sq ft)
  • Aspect ratio: 10.9:1
  • Airfoil: Wortmann FX-71-L-150/25
  • Empty weight: 265 kg (584 lb)
  • Gross weight: 385 kg (849 lb)

Performance

  • Maximum speed: 324 km/h (201 mph, 175 kn)
  • Stall speed: 80 km/h (50 mph, 43 kn)
  • g limits: +/-10g
  • Maximum glide ratio: 25:1
  • Rate of sink: 0.89 m/s (175 ft/min)
  • Wing loading: 33.36 kg/m2 (6.83 lb/sq ft)

See also edit

Aircraft of comparable role, configuration, and era

Related lists

References edit

  1. ^ a b c d Activate Media (2006). . Archived from the original on 29 August 2012. Retrieved 10 August 2011.
  2. ^ Lednicer, David (2010). . Archived from the original on 20 April 2010. Retrieved 1 August 2011.
  3. ^ Staff (December 1990). "Celstar Export Makes History". Flight International. Retrieved 10 August 2011.
  4. ^ Federal Aviation Administration (August 2011). "Make / Model Inquiry Results". Retrieved 10 August 2011.
  5. ^ https://www.sac.ca/index.php/en/free-flight-magazine-2/1980s/1989/151-ff1989-06/file
  6. ^ https://www.sac.ca/index.php/en/free-flight-magazine-2/1980s/1989/151-ff1989-06/file

External links edit

  • Celstar three view and photo

celair, celstar, south, african, wing, single, seat, aerobatic, glider, that, designed, pieter, celliers, produced, company, celair, limited, celstarrole, glidernational, origin, south, africamanufacturer, celair, limiteddesigner, pieter, celliersfirst, flight. The Celair GA 1 Celstar is a South African mid wing single seat aerobatic glider that was designed by Pieter Celliers and produced by his company Celair Pty Limited 1 GA 1 CelstarRole GliderNational origin South AfricaManufacturer Celair Pty LimitedDesigner Pieter CelliersFirst flight 1989Status Production completedNumber built At least eight Contents 1 Design and development 2 Operational history 3 Specifications GA 1 4 See also 5 References 6 External linksDesign and development editThe GA 1 was especially intended for flying competitive glider aerobatics and the resulting airframe was designed to Joint Aviation Requirements 22 standards and stressed to 10 g 1 The aircraft is made from a combination of fibreglass and aramid Its 11 2 m 36 7 ft span wing employs a Wortmann FX 71 L 150 25 airfoil The ailerons are full span and mass balanced Dive brakes are used for approach control 1 2 At least eight were produced with two exported to Switzerland and six to the United States 3 Operational history editIn August 2011 there were two GA 1s registered in the US with the Federal Aviation Administration US registered aircraft are in the Experimental Racing Exhibition category 4 Specifications GA 1 editData from Sailplane Directory 1 General characteristicsCrew one Wingspan 11 2 m 36 ft 9 in Wing area 11 54 m2 124 2 sq ft Aspect ratio 10 9 1 Airfoil Wortmann FX 71 L 150 25 Empty weight 265 kg 584 lb Gross weight 385 kg 849 lb Performance Maximum speed 324 km h 201 mph 175 kn Stall speed 80 km h 50 mph 43 kn g limits 10g Maximum glide ratio 25 1 Rate of sink 0 89 m s 175 ft min Wing loading 33 36 kg m2 6 83 lb sq ft See also editAircraft of comparable role configuration and era Allstar SZD 59 Glasflugel H 101 Pilatus PC 11 AF Swift S 1Related lists List of glidersReferences edit a b c d Activate Media 2006 GA 1 Celstar Celair Archived from the original on 29 August 2012 Retrieved 10 August 2011 Lednicer David 2010 The Incomplete Guide to Airfoil Usage Archived from the original on 20 April 2010 Retrieved 1 August 2011 Staff December 1990 Celstar Export Makes History Flight International Retrieved 10 August 2011 Federal Aviation Administration August 2011 Make Model Inquiry Results Retrieved 10 August 2011 https www sac ca index php en free flight magazine 2 1980s 1989 151 ff1989 06 file https www sac ca index php en free flight magazine 2 1980s 1989 151 ff1989 06 fileExternal links editCelstar three view and photo Retrieved from https en wikipedia org w index php title Celair GA 1 Celstar amp oldid 1211848021, wikipedia, wiki, book, books, library,

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