Paraavis Acrobat

The Acrobat was designed as an intermediate glider.^[1]

The Acrobat 26's 11.30 m (37.1 ft) span wing has 42 cells, a wing area of 24 m² (260 sq ft) and an aspect ratio of 4.9:1. The crew weight range is 70 to 90 kg (154 to 198 lb).^[1]

Data from Bertrand^[1]

General characteristics

• Crew: one
• Wingspan: 11.30 m (37 ft 1 in)
• Wing area: 24 m² (260 sq ft)
• Aspect ratio: 4.9:1

Performance

• Maximum speed: 53 km/h (33 mph, 29 kn)
• Rate of sink: 1.2 m/s (240 ft/min)