THE GAME CHANGER
Fusing 2-liner feeling with an EN C certification, the Flow Fusion is the first certified hybrid 3-2 liner paraglider.
Feel connected like a 2-line race machine, with rear riser steering on crafted control toggles, but maintain the security and comfortable workload of an EN C glider. An optimised line configuration and unique risers enable a three-line layout in the centre of the span and a two-line layout at the tips. The resulting reduction in drag increases performance noticeably.
Careful attention in the design phase has led to exceptional thermic handling bringing the composure of 2-liners to the EN C class. The tension across the span produces a more composed glider and maintains energy in the turn that enables the Fusion to carve through the sky. Surf effortlessly to cloud base and then race away efficiently on bar.
A pitch stable aerofoil, less prone to collapses and oscillations, enables the pilot to concentrate on conditions and decision making with a mind freed from micromanaging the glider. The modest aspect ratio and cell count mean a comfortable level of workload as expected for an EN C glider. The shark nose profile, 3D panel shaping and detailed internal structure combine to produce a modern sports class wing.
At speed, the Fusion risers allow the pilot to fly the glider by changing the angle of attack whilst not distorting the profile. The two-liner style risers allow the Fusion to cut through the turbulence more efficiently so that the pilot can enjoy more accessible performance throughout the speed range.
“I wanted to bring the performance of our highly successful two-line projects, the XCRacer and Spectra, to the EN C class. This Fusion has produced an accessible package that is a dream to fly and one of the most pleasant gliders I’ve ever flown.”
Felipe Rezende (Flow Designer).
TECHNICAL DATA
S
FLAT AREA
PROJECTED AREA
FLAT WINGSPAN
PROJECTED SPAN
ASPECT RATIO
PROJECTED AR
MAX CHORD
NUMBER OF CELLS
GLIDER WEIGHT
TAKE OFF WEIGHT
CERTIFICATION
M
FLAT AREA
PROJECTED AREA
FLAT WINGSPAN
PROJECTED SPAN
ASPECT RATIO
PROJECTED AR
MAX CHORD
NUMBER OF CELLS
GLIDER WEIGHT
TAKE OFF WEIGHT
CERTIFICATION
ML
FLAT AREA
PROJECTED AREA
FLAT WINGSPAN
PROJECTED SPAN
ASPECT RATIO
PROJECTED AR
MAX CHORD
NUMBER OF CELLS
GLIDER WEIGHT
TAKE OFF WEIGHT
CERTIFICATION
L
FLAT AREA
PROJECTED AREA
FLAT WINGSPAN
PROJECTED SPAN
ASPECT RATIO
PROJECTED AR
MAX CHORD
NUMBER OF CELLS
GLIDER WEIGHT
TAKE OFF WEIGHT
CERTIFICATION
MATERIALS
CANOPY
FABRIC CODE
SUPPLIER
CANOPY
FABRIC CODE
SUPPLIER
CANOPY
FABRIC CODE
SUPPLIER
CANOPY
FABRIC CODE
SUPPLIER
CANOPY
FABRIC CODE
SUPPLIER
CANOPY
FABRIC CODE
SUPPLIER
SUSPENTION LINES
FABRIC CODE
Edelrid 9200 030kg
SUPPLIER
SUSPENTION LINES
FABRIC CODE
Edelrid 9200 030kg
SUPPLIER
SUSPENTION LINES
FABRIC CODE
Liros DSL 140kg
SUPPLIER
LIROS GmbH
RISERS
FABRIC CODE
Connectors
RISERS
FABRIC CODE
Connectors
RISERS
FABRIC CODE
Connectors
ADVANCE INTERNAL STRUCTURE TENSIONING – AIST
Spanwise and chordwise precision tensioning
SHORT STRUCTURAL NYLON RODS
Fusion’s plastic rods are mostly of a short length allowing an easy fold without the use of a dedicated folding pillow. Ultimately allowing an uncomplicated folding procedure.
HYBRID 3 TO 2-LINE LAYOUT
to the traditional 3 lines layout. Ultimately translating to increased gains in performance.
- Better glide
- More solidity
- More efficiency
- Higher top-end speed
- Increased solidity at higher speeds
ALIGHTED UNDISTURBED AIR FLOW
The canopy twist and washout on the wingtips further reduce drag and improve the lift coefficients and aerodynamics on the Fusion.
PITCH STABLE SHARK NOSE AIRFOIL
Our solid shark nose profile is a pitch stable airfoil which means:
- Fewer oscillations
- More efficient glides
- Solidity at higher speeds
- Higher Comfort
OPTIMIZED INTERNAL STRUCTURE
The result is a canopy with less attachment points but more taught and rigid offering just enough flex characteristics to give the ideal feedback.
A well-tensioned sail is especially important at higher speeds to improve solidity and resistance against collapses.