Gin Falcon (Intermediate, Reflex)


Speed and efficiency without compromise
The Falcon is a state-of-the-art reflex paramotor wing for intermediate to advanced pilots. The wing is fast, stable, agile and fuel-efficient—ideal for fun flying, cross-country, bivouac and competition.

Fast and fuel-efficient
The Falcon has a wide speed range, and transitions easily from flat, efficient turns in thermals to relaxed, high-speed cruising. The wing is equipped with a competition speed system which acts on both the accelerator and the trimmer. Pushing the speedbar also simultaneously releases the trimmers and vice versa.

The Falcon also achieves excellent fuel-efficiency thanks to the aerodynamic efficiency of the state-of-the-art airfoil.

Stable and safe
The Falcon inflates easily and quickly produces lift in a coordinated manner, allowing stress-free launches in the widest range of wind speeds. The wing has a high degree of passive safety both in turbulent air and at speed. However, pilots with more limited experience must always remain aware at high speeds.

Agile and fun
Handling was a key consideration in the design and development of the Falcon. Hours of testing, tuning and trimming have resulted in an agile and precise wing. The standard steering system makes control easy and efficient, and the wing can be tip-steered at speed. Alternatively, an optional 2D steering system is available.

Overall, the Falcon is simply an all-round pleasure to fly. Whether you're drifting leisurely across the landscape or eating up the miles in a distance competition, it's a wing we believe you'll come to love.

Technical details:

  • Reflex airfoil
  • Advanced speed system
  • Easy steering system or optional 2D-steering system
  • Torque Effect Adjuster
  • Highest quality materials used throughout ensure maximum durability








FLAT AREA (m2) 20.36 22.27 24.16 26.03 27.97
SPAN (m) 10.60 11.09 11.55 11.99 12.43
ASPECT RATIO 5.5 5.5 5.5 5.5 5.5
PROJECTED AREA (m2) 17.60 19.25 20.88 22.50 24.18
SPAN (m) 8.63 9.03 9.40 9.76 10.11
ASPECT RATIO 4.2 4.2 4.2 4.2 4.2
CHORD (m)   2.43 2.54 2.65 2.75 2.85
CELL NUMBER 56 56 56 56 56
GLIDER WEIGHT (kg) 5.1 5.4 5.7 6.2 6.5
WEIGHT IN FLIGHT (kg) 75~120 85~130 95~140 105~155 115~170