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Stern ST 87 Vega

The Stern ST 87 Vega (sometimes ST-87) is a French homebuilt aircraft that was designed by Rene Stern, first flying in July 1992. The aircraft is supplied in the form of plans for amateur construction.[1]

ST 87 Vega
Role Homebuilt aircraft
National origin France
Designer Rene Stern
First flight July 1992
Status Plans available (2014)
Number built 2 (1998)

Design and development edit

The ST 87 Vega features a cantilever low-wing, a two-seats-in-side-by-side configuration enclosed cockpit under a bubble canopy, fixed conventional landing gear with wheel pants and a single engine in tractor configuration.[1]

The aircraft is made from wood, with its flying surfaces covered in doped aircraft fabric. Its 7.62 m (25.0 ft) span wing mounts flaps and has a wing area of 10.0 m2 (108 sq ft). The cabin width is 110 cm (43 in). The acceptable power range is 85 to 125 hp (63 to 93 kW) and the standard engine used is the 108 hp (81 kW) Lycoming O-235 powerplant.[1]

The ST 87 Vega has a typical empty weight of 469 kg (1,034 lb) and a gross weight of 726 kg (1,601 lb), giving a useful load of 257 kg (567 lb). With full fuel of 110 litres (24 imp gal; 29 US gal) the payload for the pilot, passenger and baggage is 175 kg (386 lb).[1]

The manufacturer estimates the construction time from the supplied kit as 2000 hours.[1]

Operational history edit

By 1998 the company reported that four kits had been sold and two aircraft were completed and flying.[1]

Specifications (ST 87 Vega) edit

Data from AeroCrafter[1]

General characteristics

  • Crew: one
  • Capacity: one passenger
  • Wingspan: 7.62 m (25.00 ft)
  • Wing area: 10.0 m2 (108 sq ft)
  • Empty weight: 469 kg (1,035 lb)
  • Gross weight: 726 kg (1,600 lb)
  • Fuel capacity: 110 litres (24 imp gal; 29 US gal) standard, a total of 260 litres (57 imp gal; 69 US gal) optional
  • Powerplant: 1 × Lycoming O-235 four cylinder, air-cooled, four stroke aircraft engine, 81 kW (108 hp)
  • Propellers: 2-bladed metal fixed pitch

Performance

  • Maximum speed: 240 km/h (150 mph, 130 kn)
  • Cruise speed: 201 km/h (125 mph, 109 kn)
  • Stall speed: 80 km/h (50 mph, 43 kn) flaps down
  • Range: 1,210 km (750 mi, 650 nmi)
  • Service ceiling: 4,000 m (13,000 ft)
  • Rate of climb: 3.6 m/s (700 ft/min)
  • Wing loading: 72 kg/m2 (14.8 lb/sq ft)

References edit

  1. ^ a b c d e f g Purdy, Don: AeroCrafter - Homebuilt Aircraft Sourcebook, Fifth Edition, page 200. BAI Communications, 15 July 1998. ISBN 0-9636409-4-1

External links edit

  • Photo of a Stern ST 87 Vega

stern, vega, sometimes, french, homebuilt, aircraft, that, designed, rene, stern, first, flying, july, 1992, aircraft, supplied, form, plans, amateur, construction, vegarole, homebuilt, aircraftnational, origin, francedesigner, rene, sternfirst, flight, july, . The Stern ST 87 Vega sometimes ST 87 is a French homebuilt aircraft that was designed by Rene Stern first flying in July 1992 The aircraft is supplied in the form of plans for amateur construction 1 ST 87 VegaRole Homebuilt aircraftNational origin FranceDesigner Rene SternFirst flight July 1992Status Plans available 2014 Number built 2 1998 Contents 1 Design and development 2 Operational history 3 Specifications ST 87 Vega 4 References 5 External linksDesign and development editThe ST 87 Vega features a cantilever low wing a two seats in side by side configuration enclosed cockpit under a bubble canopy fixed conventional landing gear with wheel pants and a single engine in tractor configuration 1 The aircraft is made from wood with its flying surfaces covered in doped aircraft fabric Its 7 62 m 25 0 ft span wing mounts flaps and has a wing area of 10 0 m2 108 sq ft The cabin width is 110 cm 43 in The acceptable power range is 85 to 125 hp 63 to 93 kW and the standard engine used is the 108 hp 81 kW Lycoming O 235 powerplant 1 The ST 87 Vega has a typical empty weight of 469 kg 1 034 lb and a gross weight of 726 kg 1 601 lb giving a useful load of 257 kg 567 lb With full fuel of 110 litres 24 imp gal 29 US gal the payload for the pilot passenger and baggage is 175 kg 386 lb 1 The manufacturer estimates the construction time from the supplied kit as 2000 hours 1 Operational history editBy 1998 the company reported that four kits had been sold and two aircraft were completed and flying 1 Specifications ST 87 Vega editData from AeroCrafter 1 General characteristicsCrew one Capacity one passenger Wingspan 7 62 m 25 00 ft Wing area 10 0 m2 108 sq ft Empty weight 469 kg 1 035 lb Gross weight 726 kg 1 600 lb Fuel capacity 110 litres 24 imp gal 29 US gal standard a total of 260 litres 57 imp gal 69 US gal optional Powerplant 1 Lycoming O 235 four cylinder air cooled four stroke aircraft engine 81 kW 108 hp Propellers 2 bladed metal fixed pitchPerformance Maximum speed 240 km h 150 mph 130 kn Cruise speed 201 km h 125 mph 109 kn Stall speed 80 km h 50 mph 43 kn flaps down Range 1 210 km 750 mi 650 nmi Service ceiling 4 000 m 13 000 ft Rate of climb 3 6 m s 700 ft min Wing loading 72 kg m2 14 8 lb sq ft References edit a b c d e f g Purdy Don AeroCrafter Homebuilt Aircraft Sourcebook Fifth Edition page 200 BAI Communications 15 July 1998 ISBN 0 9636409 4 1External links edit nbsp Wikimedia Commons has media related to Stern aircraft Photo of a Stern ST 87 Vega Retrieved from https en wikipedia org w index php title Stern ST 87 Vega amp oldid 1126751878, wikipedia, wiki, book, books, library,

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