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 YOUR MANTRA R11

5

ENGLISH

The R11 is a carefully refined evolution of the R10.2: We have striven 

to retain all of the best characteristics of the R10.2 while improv-

ing some of its issues. The R11 includes several highly innovative 

new features such as the Shark Nose. These have led to significant 

improvements in performance, comfort, and ease of use.

The main aim of the R11 project was to increase the top speed and 

improve top speed stability. We have achieved this with the help of a 

careful sail-reshaping and with the help of the new Shark Nose. The 

new profile, with the new cell opening positioning increases the inter-

nal pressure, especially at low angles of attack.

This means that not only can the R11 achieve a faster top speed 

than the R10.2 but it also remains more stable at this speed (with 

a greater resistance to collpase). The R11 is more comortable to fly, 

the sail moves less and there is less migration of air (outflow) around 

the leading edge so the internal pressure remains more constant.

Brake Lines

The main brake line lengths have been set carefully during testing, 

however, if you do choose to adjust them, please bear in mind the 

following: 

Do not reduce the set lengths, this may cause the wing to en-

• 

gage the brakes whilst at full speed.

Ensure both main brake lines are of equal length.

• 

If a brake handle has been removed, check that its line is still  

• 

routed through the pulley when it is replaced.

When  the  brake  handles  are  released  in  flight,  the  brake  lines                                               

• 

should  be  slack.  There  must  be  a  substantial  “bow”  in  them  to 

guarantee no deformation of the trailing edge. 

IMPORTANT: In the unlikely event of a brake line snapping 

in flight, or a handle becoming detached, the glider can be 

flown by gently pulling the rear risers (B-risers) for direc-

tional control.

Risers

The Mantra R11 has been designed with 2 rows of lines A & B. 

C lines are no longer necessary; they only create drag.

Each riser has a set of trimmers, these are used to slow the wing in 

thermals and to optimise the trim speed.

Total Weight in flight

Each R11 has a defined optimum weight range, it does not have to 

be flown at the top of this range for a good feel and handling, this can  

also be achieved near the bottom of the range. If you are between 

sizes the following information may help you:

If you want better speed, precise handling, and generally fly in moun-

tains and/or in strong conditions, you should chose to fly in the top 

part of the weight range. If you want a better sink rate, or if you gen-

erally fly in flat lands and/or in weak conditions, you may choose to fly 

near the bottom part of the weight range. Remember, you can always 

add ballast when conditions are stronger. 

Summary of Contents for Mantra R11

Page 1: ......

Page 2: ...YOUR WING IS HERE...

Page 3: ...CONTENTS Pilots Manual Eng 2 14 Materials 15 Line Diagram 16 Riser Diagram Lengths 17 Technical Specifications 17 Version 1 0 April 2011...

Page 4: ......

Page 5: ...rea which includes the sites of Gourdon Monaco and Lachens guarantees us more than 300 flyable days per year This is a great asset in the development of the Ozone range If you need any further informa...

Page 6: ...flying your glider in rain snow strong wind and turbulent weather conditions or clouds Remember PLEASURE is the reason for our sport Everyone at Ozone continues to be driven by our passion for flying...

Page 7: ...akes whilst at full speed Ensure both main brake lines are of equal length If a brake handle has been removed check that its line is still routed through the pulley when it is replaced When the brake...

Page 8: ...e checked lines on top of the previous set and making sure no lines are tangled knotted or snagged Mirror the process on the other side Take off checklist 1 Check reserve parachute pin in and handle s...

Page 9: ...teristics Flying with the trimmers in the fully slow position gives the best minimum sink rate Find your optimum position depending on your personal tastes wing loading and the conditions you are flyi...

Page 10: ...he brakes which causes drag and pitch movements the direct feel allows you to stop collapses before they happen and maintain higher speeds and higher levels of efficiency through turbulence To fly wit...

Page 11: ...lone will normally be enough for a full recovery of the wing In your efforts to stop the glider turning towards the collapsed side you must be very careful not to stall the side of the wing that is st...

Page 12: ...will not reinflate the wing and pumping too slow might take the glider close to or beyond the stall point Symmetrical collapses normally reinflate without pilot input how ever a quick input of 15 to 2...

Page 13: ...ed wing on Saucisse pack It is best to start from the mushroomed position as this reduces the dragging of the leading edge across the ground Step 2 Group LE reinforce ments with the A tabs aligned mak...

Page 14: ...acked away Heat and humidity are the worst factors in damag ing your glider Storing a damp glider in your car under the sun would be terrible for example Dry your wing preferably out of the sun in the...

Page 15: ...first time after 80 hrs or 12 months whichever comes sooner and there after annually The checker should inform you about the condition of your glider and whether or not any parts need to be re checked...

Page 16: ...mended service intervals this is especially important for the lines any damaged lines must be replaced at the first sign of visual damage and the whole set must be changed after 150hrs of use Finally...

Page 17: ...tex 9017 E77 Lower surface Porcher Skytex 9017 E68 Supported Internal Ribs Porcher Skytex 9017 E29A Unsupported Ribs Dominico 30D FM Leading edge reinforcement Plastic P18 P25 Line Set Lower cascade E...

Page 18: ...A6 A7 A8 A9 A10 A11 A12 A13 A14 AR1 AR2 AR3 BR1 BR2 BR3 ARU4 K1 KMU1 KMU2 KMU3 KMU4 KMU5 KMU6 K2 K3 K4 K5 K6 K7 K8 K9 K10 K11 K12 KML1 KML3 KML2 KRL MantraR11 r iggingdiag R am KRU A15 A16 AMU1 ARL4...

Page 19: ...82 82 82 82 82 82 Projected Area m2 Flat Area m2 19 5 20 7 22 23 7 25 7 27 6 Projected Span m Flat Span m Projected Aspect Ratio Flat Aspect Ratio 7 55 7 55 7 55 7 55 7 55 7 55 Root Chord Glider Weig...

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