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all aspects of flight and even in the most adverse conditions every 
pilot input is met with an immediate and precise response. Please read 
section 2.8 Adjusting the brakes.

Every adjustment of the trimmers will each time transform the wing and 
by releasing them the KOUGAR 2 will feel more pressurised and solid, 
penetrating the different layers of laminar air, absorbing turbulence 
while increasing stability and reducing the roll. Please read section 2.7 
Trimmers.

In comparison with other reflex profiles the speed/consumption ratio is 
far better with the Niviuk RSP Its cruising speed and fuel consumption 
are excellent attributes for the lovers of long journeys. If the decision is 
to fly for long periods at maximum speed then the fuel consumption will 
reflect that of other profiles.

The KOUGAR 2 has the same advantages when landing as it does on 
take-off. With a low speed approach, a short final glide and with the pilot 
always in total control the KOUGAR 2 can land in the smallest of areas 
with precision and ease. 

It is worthwhile remembering that the best paraglider in the hands of a 
bad pilot does not guarantee a happy ending. The KOUGAR 2 passive 
safety measures should also be accompanied by the passive safety 
offered by the rest of the flying equipment. The harness, helmet the 
emergency parachute etc. The extraordinary behaviour of the KOUGAR 2  
and common-sense piloting will give you many hours of peaceful flying.

1.4 ASSEMBLY, MATERIALS

The KOUGAR 2 does not only introduce new design methods but also 
new manufacture technologies. Not a single millimetre of error is possible 
in the manufacturing process from Olivier’s computer to the cutting of the 
fabric. The cutting is done section by section in an extremely meticulous 
manner. The numbering and marking of the guideline marks is also done 

in the same meticulous way so avoiding errors in this critical process.

It may be a surprise for some pilots to learn that the lines used on the 
KOUGAR 2 are not the standard larger diameter lines which are normally 
associated and used as standard on PPG wings but in fact lines similar 
in diameter to those used on classic free flying, none powered wings. 
The old argument of thicker lines equals more strength and power 
is absolutely the opposite principle to achieving efficient profiles of 
flight. Niviuk believe that every aerodynamic improvement should be 
researched, assessed and if appropriate incorporated within a design. 
The latest advances in line technology have been researched and applied 
to the KOUGAR 2 allowing lighter smaller diameter lines to be used with 
improved aerodynamic efficiency but without any reduction in strength or 
overall security. 

The lines are semi-automatically manufactured and all the sewing is 
finished under the supervision of our specialists.  The jigsaw puzzle of 
the assembly process is made easier using this method. We economise 
on resources while making the quality control more efficient. All the 
different parts of the canopy are cut and assembled under the strict 
conditions induced by the automation of the whole process. All NIVIUK 
Gliders go through an extremely thorough and efficient final inspection. 
Every single line of each glider is measured individually once the final 
assembly has concluded. 

Each wing is thoroughly inspected at the end of it assembly. Each glider 
is packaged following the maintenance and conservation instructions 
recommended for the advanced materials. 

NIVIUK Gliders are made of first class materials as demanded by the 
performance, durability, and homologation requirements of the present-
day market. 

Information about construction materials is given on the last pages of this 
manual.

Summary of Contents for Kougar-2

Page 1: ...USER S MANUAL KOUGAR 2...

Page 2: ...the first generation glider but now delivers superior maximum speed with added safety We are confident that you will enjoy flying this wing and that you will soon understand the meaning of our slogan...

Page 3: ...IGHT CHECK LIST 10 3 6 WING INFLATION CONTROL AND TAKE OFF 10 3 7 LANDING 11 4 IN FLIGHT 11 4 1 FLYING IN TURBULENCE 11 4 2 POSSIBLE CONFIGURATIONS 11 4 3 USING THE ACCELERATOR 12 4 4 FLYING WITHOUT B...

Page 4: ...viuk Reflex Profile RSP was to achieve a profile with better performance than any other current reflex profile In doing so we have applied many years of research and design knowledge with the addition...

Page 5: ...iculous manner The numbering and marking of the guideline marks is also done in the same meticulous way so avoiding errors in this critical process It may be a surprise for some pilots to learn that t...

Page 6: ...he Reflex System Profile RSP This innovation works together with the previous design to improve gliding speed and safety In addition it cuts down on fuel consumption less engine power is needed to obt...

Page 7: ...celeration system When fitting any accelerator system ensure that all preinstalled items within the harness such as roller pulleys are used correctly After fitting take into account that you will have...

Page 8: ...lowing the pilot to either increase speed by opening the trimmers or conversely decrease speed by closing them Each trimmer is equipped with a scale clearly numbered so allowing the pilot to easily ch...

Page 9: ...to meet with the certification requirements during the certification procedure However due to possible specification differences brought by various paramotor types those settings can be adjusted to me...

Page 10: ...ppropriate for your flight and the rescue system is secure and unhindered Once ready and immediately prior to takeoff a final visual check of the equipment and all attachments must be carried out Chec...

Page 11: ...nternal pressure with extraordinary leading edge rigidity at high speed The glider turns without losing its handling flexibility nor its stable flight characteristics The wing s high performance abili...

Page 12: ...orward with great energy and may result in the wing below the pilot It is very important that the pressure on the brake lines is maintained until the wing is well established vertical above Wing tangl...

Page 13: ...HEIGHT The knowledge of the different descent techniques is an important resource to use in certain situations The most adequate descent method will depend on the particular situation The following i...

Page 14: ...tic flight to be any form of piloting that is different to normal flight Extreme manoeuvres take you and your wing to centrifugal forces that can reach 4 to 5 g Materials will wear more quickly than i...

Page 15: ...it by using the rip stop found in the repair kit so long as no stitches are involved in the tear Any other type of tear must be repaired in a specialized repair shop or by qualified personnel Do not...

Page 16: ...NES TOTAL METERS M 304 327 345 362 HEI GHT M 6 75 7 25 7 55 7 99 NUMBER 182 182 182 182 MAI N 2 1 3 4 1 2 1 3 4 1 2 1 3 4 1 2 1 3 4 1 RI SERS NUMBER 4 A a B C D A a B C D A a B C D A a B C D TRI MS m...

Page 17: ...UPPER CASCADES TNL 80 TEIJIM LIMITED JAPAN UPPER CASCADES DC 060 LIROS GMHB GERMANY UPPER CASCADES DC 040 LIROS GMHB GERMANY MIDDLE CASCADES TNL 140 TEIJIM LIMITED JAPAN MIDDLE CASCADES TNL 80 TEIJIM...

Page 18: ...18 11 3 RISERS PLAN...

Page 19: ...19 11 4 SUSPENSION PLAN...

Page 20: ...m m A B C D 480 480 480 480 STANDARD 480 525 570 615 TRI MMER OPENED 300 395 480 565 ACCELERATED KOUGAR 2 2 0 LI NES HEI GHT m m A B C D br 1 6675 6582 6646 6920 7426 2 6589 6497 6546 6725 7186 3 660...

Page 21: ...m m A B C D 480 480 480 480 STANDARD 480 525 570 615 TRI MMER OPENED 300 395 480 565 ACCELERATED LI NES HEI GHT m m KOUGAR 2 2 5 A B C D br 1 7411 7307 7377 7681 8219 2 7319 7217 7270 7469 7957 3 734...

Page 22: ...KOUGAR 2 20 KOUGAR 2 23 22 11 9 CERTIFICATION SPECIMEN TEST...

Page 23: ...KOUGAR 2 25 KOUGAR 2 28 23...

Page 24: ...The importance of small details niviuk com...

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