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NIVIUK - ICEPEAK X ONE
New
Leader of the pack
A greater speed range combined with an impeccable and efficient glide will allow you to be one step ahead of the rest in all competitions.
The perfect balance
A modern design and a new airfoil facilitated the creation of a fast, solid and performant wing during all phases of flight.
INFORMATION FROM MANUFACTURER WEBSITE
TARGET & ADVANTAGES
CCC
Stand out in all competitions with the best possible performance. A fast and versatile wing that will allow you to get the best results.
Top performance
- Increased top speed.
- Improved glide in all conditions.
- Improved glide in all conditions.
In flight
- The X-One is a wing that is easy to master.
- More efficient steering with the B risers: when under pressure, it allows easier and more controlled steering when reaching maximum speed. Turning is much easier in any conditions.
High level of comfort
- Despite its significant aspect ratio, it is a very compact wing.
Niviuk Technologies
The perfect finish
A cleaner leading edge with fewer creases in order to reduce drag. It features an optimised trailing edge with more reinforcements and a new construction method of the wing surface.
New profile
The wing has been optimised to achieve better lift for more performance in all flight conditions and to allow higher top speeds.
16 more cells than the Evox
Adding extra cells has made the wing surface cleaner. Even with increased aspect ratio, the wing is more compact.
Wing twist
With a new wing twist adjustment, the Icepeak X-One is much safer, has more gentle reactions and more speed.
New internal structure
A new internal structure guarantees a better load distribution.
New aspect ratio - 8
The highest aspect ratio Niviuk has ever had in a certified wing.
New risers
The optimisation of the risers allows for a much more progressive acceleration.
New Ergo handle
The new Ergo handles make steering more intuitive and efficient especially at high speed.
Technical data
20 | 22 | 24 | 25 | 26 | |||
CELLS | NUMBER | 115 | 115 | 115 | 115 | 115 | |
ASPECT RATIO | FLAT | 8 | 8 | 8 | 8 | 8 | |
AREA | FLAT | m² | 20 | 21,7 | 23 | 24,6 | 26,4 |
PROJECTED | m² | 17,07 | 18,52 | 19,63 | 20,9 | 22,53 | |
CHORD | MAXIMUM | m | 1,98 | 2,06 | 2,12 | 2,19 | 2,27 |
LINES | NUMBER | m | 197 | 205 | 211 | 219 | 227 |
MAIN | 1+1+1/3 | 1+1+1/3 | 1+1+1/3 | 1+1+1/3 | 1+1+1/3 | ||
RISERS | NUMBER | A+A´+A´´/B | A+A´+A´´/B | A+A´+A´´/B | A+A´+A´´/B | A+A´+A´´/B | |
SPEED-BAR | mm | 140 | 140 | 140 | 140 | 140 | |
TOTAL WEIGHT IN FLIGHT | kg | 80-95 | 90-105 | 98-112 | 108-120 | 118-130 | |
GLIDER WEIGHT | kg | 5,9 | 6,06 | 6,32 | 6,65 | 6,91 | |
OPT. WEIGHT IN FLIGHT | kg | 88 - 91 | 100 - 101 | 108 - 109 | 117 - 119 | 128 - 130 | |
CERTIFICATION | CCC | CCC | CCC | CCC | CCC |
| Sertifikācija | CCC |
