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Advanced Soaring Concepts Spirit

American glider From Wikipedia, the free encyclopedia

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The Advanced Soaring Concepts Spirit, also called the Advanced Soaring Concepts American Spirit, is an American mid-wing, T-tailed. single-seat, FAI Standard Class glider that was designed by Tor Jensen and produced by Advanced Soaring Concepts, first flying in 1992. The aircraft was produced in kit form for amateur construction.[1][2]

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Design and development

The Spirit was the Standard Class design that paralleled the company's FAI 15-Metre Class Falcon.[1][2]

The aircraft is made from a welded steel tubing, with an Aramid reinforced cockpit section. Its 15 m (49.2 ft) span wing employs a Carbon-fiber-reinforced polymer spar and carbon sandwich construction. The kit came with pre-molded fiberglass parts. The cockpit was designed to accommodate a pilot of up to 76 in (193 cm) in height and weighing up to 260 lb (118 kg) with parachute.[1][2]

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Specifications (Spirit)

Data from Purdy and Sailplane Directory[1][2]

General characteristics

  • Crew: one
  • Wingspan: 49 ft 3 in (15 m)
  • Wing area: 101.1 sq ft (9.39 m2)
  • Aspect ratio: 23.9:1
  • Empty weight: 508 lb (230 kg)
  • Gross weight: 1,160 lb (526 kg)

Performance

  • Stall speed: 44 mph (71 km/h, 38 kn)
  • Maximum glide ratio: 44:1
  • Wing loading: 11.47 lb/sq ft (56.0 kg/m2)
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See also

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References

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