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during landing must be decreased by using the brakes and if necessary 
by a longer run off as the pilot makes contact with the ground 

When landing in moderate wind conditions, the ground speed is reduced 
so simple and progressive application of the brakes will be enough for a 
perfect landing. Landing with open or half open trimmers is possible, but 
it will be necessary to balance the application of the brakes to the position 
of the trimmers and the forward ground speed being experienced. Of 
course open trimmers and an increase in forward ground speed when 
landing may require a larger landing area as opposed to when the 
trimmers are closed.  

The KOUGAR 2 very efficiently transforms forward speed into lift and 
inherently allows a wide margin for error either with or without wind.

4. IN FLIGHT

It is important to stress that the reaction to the manoeuvres is different in 
each wing size, and even the reactions and solutions to each manoeuvre 
are different on the same size wing when the overall loading (i.e. Pilot/
harness Weight/ wing load).
 
Having known the aforementioned facts, pilots will be able to face 
different situations more appropriately. The greater the wing loading, the 
lesser the incidence rate; but the glider will react more abruptly.  
In terms of piloting the wing, the main toggles are more flexible and 
progressive, enabling for better glider control without excessive effort. 
An additional toggle system, connected to the stabilizer, improves glider 
management during accelerated flights and turns.

The KOUGAR 2 can be steered with the trims opened while keeping the 
profile stable. In other words; maintaining a high wing internal 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 abilities enhance the engine’s power curve 
for a lesser workload, enabling the use of smaller size 125 and 80 cc. 
motors and without the need for high cubic capacity power plants.

4.1 FLYING IN TURBULENCE

The KOUGAR 2 comfortably absorbs moderate turbulence in either 
normal or accelerated flight, minimising any bouncing effect which is 
often experienced with other reflex profiles. 
Over handling

Most flying incidents are caused by incorrect actions of the pilot, which 
chained one after another creates abnormal flying configurations (a 
cascade of incidents). You must to remember that over handling the 
wing will lead to critical levels of functioning. The KOUGAR 2 is designed 
always to try to recover normal flight by itself, do not try to over handle it.

Generally speaking, the reactions of the wing, which follow over handling, 
are neither due to the input made or the intensity, but the length of time 
the pilot continues to over handle. You have to allow the profile to re-
establish normal flight speed after any type of handling.

The most important safety and security feature of every glider is the pilot.

4.2 POSSIBLE CONFIGURATIONS

The following indications should be viewed as purely informative, solely 
relevant to normal flying settings, and can not to be considered nor 
viewed as a paragliding teaching manual. Only professional paragliding 
schools can teach and prepare pilots to do all these maneuvers. 

Asymmetric collapse
The collapse will normally open by itself but if that does not happen, pull 
completely on the brake line on the side, which has collapsed. Do this 
with a firm movement. You may have to repeat this operation to provoke 

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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