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smooth, even when fully accelerated. During glides, the wing maintains 
altitude and the wing remains stable. Improved turn precision means 
handling is less physical and provides better feedback. Inflating the wing 
is much easier and gentler, without overshooting.

Flying this wing is very intuitive, with clear and useful feedback about the 
air mass. It responds to the pilot’s inputs effectively and even in thermic 
and turbulent conditions it remains stable and solid.

The PEAK 5 flies efficiently. It enters thermals with sufficient speed to 
centre in the lift and climbs progressively.  The handling is progressive 
and effective for even more flying pleasure under an exciting wing of 
extraordinary quality.   

It is lightweight; even lighter in flight and easy to pilot, with outstanding 
turbulence buffering and a surprising range of speed for incredible glides.

1.4 ASSEMBLY, MATERIALS

The PEAK 5 has all the technological innovations used on other Niviuk 
gliders and is built with the most careful selection of current materials. It 
has all the current technology and accessories available to improve pilot 
comfort whilst increasing safety and performance.
In the design of all Niviuk products the team aims to ensure development 
and continuous improvement. The technologies developed in recent 
years have allowed us to develop greater, better wings. It is in this 
context that we would like to introduce the technologies included in this 
new model. 

RAM Air Intake

 - this system is characterised by the arrangement of the 

air inlets, to ensure optimal maintenance of internal pressure. Thanks to 
this design, we were able to reduce their size, while maintaining the same 
air flow at all angles to improve laminar flow. More consistency across 
the whole speed range and better performance without compromising on 
safety.

Titanium Technology (TNT)

 - a revolutionary technique using titanium. 

Using Nitinol in the internal construction provides a more uniform profile 
and reduces the weight to gain efficiency in flight. Nitinol provides the 
highest level of protection against deformation, heat or breaks. The 
leading edge is more rigid and the wing surface remains perfectly taut, 
without creases or parasitic drag.  This optimises glide in all phases of 
the flight.  Because the flexible rods always return to their original shape, 
the integrity of the profile is never affected.  Nitinol provides the highest 
level of protection against deformation, heat or breaks.

Structured Leading Edge (SLE)

 - the use of the SLE considerably 

reduces the amount of Mylar which was used in previous Niviuk wings 
and this also reduces the weight of the leading edge. Therefore it is 
easier to inflate this wing than a paraglider without this system.

3D Pattern Cut Optimisation (3DP)

 – the latest generation of wings 

require a new fabric panel pattern and cutting system. Creating separate 
panels for each of the sections at the front of the wing means the sail 
fabric is more taut and crease-free. During the cutting, the optimal 
orientation of the fabric section is selected, depending on its final 
location. If the fabric pattern is properly aligned with the axes of load, it 
suffers less deformation after repeated use, to the long-term benefit of 
the leading edge.

3D Leading Edge (3DL)

 - adding an extra seam to the longitudinal 

axis of the glider helps, on the one hand, give more consistency and 
volume to the profile (a more efficient 3D contour) and on the other, joins 
and shapes the leading edge panels. The fabric is guided by the panel 
position to ensure fewer creases and better load distribution. The result 
is a cleaner profile, which benefits the wing in terms of performance and 
durability.

Structured Trailing Edge (STE)

 - optimises the profile without deforming 

it. The circulation of the air is more fluid, ensuring a cleaner airflow.  
When changing the angle of attack or when accelerated, the profile 

Summary of Contents for PEAK 5

Page 1: ...PEAK 5 User s manual...

Page 2: ...glider and will soon discover the meaning of our motto The importance of small details This is the user manual and we recommend you read it carefully The NIVIUK Gliders Team USER S MANUAL NIVIUK Glid...

Page 3: ...0 3 7 PACKING 10 4 IN FLIGHT 10 4 1 FLYING IN TURBULENCE 10 4 2 POSSIBLE CONFIGURATIONS 10 4 3 ACCELERATED FLIGHT 13 4 4 FLYING WITHOUT BRAKE LINES 13 4 5 KNOT S IN FLIGHT 13 5 LOSING ALTITUD 13 5 1 B...

Page 4: ...ents of the test pilot The report contains all the necessary information on how the paraglider reacts during each of the tested manoeuvres It is important to note that different size wings will react...

Page 5: ...TNT a revolutionary technique using titanium Using Nitinol in the internal construction provides a more uniform profile and reduces the weight to gain efficiency in flight Nitinol provides the highes...

Page 6: ...ine diameter has been calculated depending on the workload and aims to achieve the required best performance with the least drag The sheath protects the line cores from UV rays and abrasions The lines...

Page 7: ...IKS or carabiners are properly fastened and securely locked PLEASE NOTE The PEAK 5 features risers of different lengths Size 21 uses risers of unequal lengths In all other models the risers are equal...

Page 8: ...will fly at maximum speed but the glide will be adversely affected Released speed bar the A and B risers are aligned Full speed bar Size 21 13 cm Sizes 22 24 and 26 14 cm Please note The use of the s...

Page 9: ...is advisable to fly with the original setting for a period of time to get used to the actual behaviour of the PEAK 5 In case it is necessary to modify the brake length loosen the knot slide the line...

Page 10: ...ect the integrity of the wing over time Make sure the reinforcements are not bent or folded It should not be folded too tightly to avoid damage to the cloth and or lines At Niviuk we have designed the...

Page 11: ...g light brake pressure to that side if necessary Normally the collapsed side of the wing should then recover and reopen by itself If it does not try to weight shift towards the collapsed side If this...

Page 12: ...handles down to bring the wing back up and release them immediately while the glider is still in transition to reposition itself overhead Cravat A cravat may happen after an asymmetric collapse when...

Page 13: ...ed by weight shifting to the opposite side and applying a slight brake pull to that side Gently pull the brake line to see if the knot can be undone or try to locate the problem line Try pulling it to...

Page 14: ...ears This new rapid descent technique was first discovered by our Niviuk team pilots in 2009 while flying a competition prototype wing which because of its line plan and high aspect ratio would not al...

Page 15: ...ly experience an asymmetrical acceleration and dive depending on how the manoeuvre was carried out Practise these manoeuvres at sufficient altitude and carefully 5 5 SLOW DESCENT TECHNIQUE This techni...

Page 16: ...f your wing is wet from contact with water place it in a dry area air it and keep it away from direct sunlight Direct sunlight may damage the wing s materials and cause premature aging After landing d...

Page 17: ...d from another wing of the same type Each trim setting is individual to each wing and is determined after measurements and subsequent analysis by specialist personnel Trim adjustments must be within 1...

Page 18: ...tification The following are not considered to be modifications a replacement of damaged parts b trim correction c repairs d partial or total line replacement The above must all be carried out accordi...

Page 19: ...0 211 2 1 3 2 1 3 2 1 3 2 1 3 2 1 A A B A A B A A B A A B mm 130 140 140 140 Kg 70 85 80 98 92 110 105 125 Kg 5 5 3 5 5 5 8 D D D D 10 TECHNICAL DATA 10 1 TECHNICAL DATA 20 CELLS Number ASPECT RATIO F...

Page 20: ...OS GMHB GERMANY UPPER CASCADES DC 35 LIROS GMHB GERMANY UPPER CASCADES A 8000 U 50 EDELRID GERMANY UPPER CASCADES A 8000 U 70 EDELRID GERMANY MIDDLE CASCADES DC 35 LIROS GMHB GERMANY MIDDLE CASCADES A...

Page 21: ...10 3 RISERS PLAN 22...

Page 22: ...10 4 SUSPENSION PLAN 23...

Page 23: ...00 500 360 405 500 A B C D BR 1 7238 7203 7223 7309 7562 2 7145 7107 7111 7197 7301 3 7120 7082 7088 7173 7194 4 7149 7115 7146 7224 7242 5 7055 7022 7024 7091 7054 6 6923 6892 6897 6959 6863 7 6848 6...

Page 24: ...00 500 360 405 500 A B C D BR 1 8067 8030 8052 8147 8490 2 7966 7926 7931 8027 8201 3 7941 7901 7909 8003 8083 4 7977 7942 7976 8063 8139 5 7874 7839 7843 7918 7931 6 7731 7697 7704 7773 7719 7 7648 7...

Page 25: ...C 5 A 6 A 7 A 8 A 9 D 10 D 11 A 12 A 13 A 14 D 15 A 16 A 17 A 18 B 19 0 20 A 21 A 22 A 23 0 Classification D In accordance with standards EN 926 1 2015 EN 926 2 2013 and LTF NFL II 91 09 PG_1611 2019...

Page 26: ...B 4 C 5 A 6 A 7 A 8 A 9 D 10 D 11 A 12 A 13 C 14 D 15 A 16 A 17 A 18 B 19 0 20 B 21 B 22 A 23 0 Classification D In accordance with standards EN 926 1 2015 EN 926 2 2013 and LTF NFL II 91 09 PG_1673 2...

Page 27: ...niviuk com...

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