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12

11

Recovery

Release the riser at first rapidly but then gently. After the B-line stall on no account just let 
go of the B-risers, as this can cause overloading. As soon as the risers have been 
released, the MUSE II will usually fly normally of its own accord. Otherwise you have two 
possibilities:

1. Pull the A-risers, until the canopy regains forward speed. 

 Don't pull too far, 

or a frontal tuck will develop.

2. Pull the brake lines until the canopy wants to fall backwards, and then instantly open 

both brakes symmetrically. As a result the canopy will shoot forwards, thus regaining 
forward speed.

So begin with option 1, and only rely on option 2 when you have enough experience with 
the manoeuvre.

If you find yourself in an unintentional spin and you are high enough, you should:
1. Release the brakes immediately. The glider will stop rotating, if it does not apply 

sufficient outside brake to stop rotation.

2. Gently apply the brakes to avoid a central collapse of the canopy and the possibility of 

a cravat (one of the tips becoming entangled in the lines).

This is included only to expand your knowledge of how the canopies performance. Not 
recommended as a descent technique.

Initiation

Take wraps until the glider is lightly braked (when the hands are right up). Now gently pull 
both brake lines, until the canopy falls away behind - at this point, dynamically pull the 
brakes fully down. Press your hands against your body. The glider is now over you, with 
the wing tips flapping. As a result you sink rapidly with no forward movement.

WARNING!

NOTE!!

 In the case of a cravat which pumping of the brakes fails to release - apply 

50% - 70% brake on the open side of the canopy to stop rotation. Then pull the caught 
line carefully to release it then pump out the affected side.

WARNING!!

 If you are LOW and are in an unintentional spin, or if the canopy is caught in 

a cravat USE YOUR RESERVE.

Spin (negative spirals)

Full stall

Stalls

Turbulence or rapid braking can lead to a pendulum effect, and thus to changes in the 
angle of attack. In extreme cases this can make the airflow break away from the upper 
surface of the canopy even without the brakes being activated.

Initiation

Pull the brakes slowly down until you have no more forward speed. The canopy now 
loses internal pressure and the lower surface pushes further and further up between the 
suspension points. The loss of internal pressure is greater the longer the glider is held in 
this situation. During the parachutal stall the canopy always remains open.
You will probably have to feel for the right brake position at first. If you apply too much 
brake, the canopy falls away backwards and the glider finds itself on the brink of a full 
stall. Loosen the brake lines immediately, until the canopy is once more above you. If you 
hesitate too long, the canopy will surge forwards. 

Recovery

As soon as you release both brakes, symmetrically, the glider will independently recover 
from the parachutal stall.

Initiation

Put your hands through the brake handles and grip the B-risers at the height of the 
maillons. Now pull the B-risers slowly down, until the canopy folds (parallel to its long 
axis). The glider will now stabilise itself and sink rapidly, with virtually no forward speed. 
Keep hold of the B-risers throughout the manoeuvre.

WARNING!!

 All canopies need some time after a stall (in extreme cases a couple of 

seconds) before the airflow builds up again. You should therefore carry out all 
manoeuvres involving stalls at an adequate height, as it will take a certain amount of time 
before the glider flies with its normal sink rate.

WARNING!!

 In a parachutal stall, asymmetrical application of the brakes can lead to a 

spin. If you must land from a parachutal stall, on no account apply the brakes very close 
to the ground, as a reduction in area increases the descent rate.

Parachutal stall with steering lines

B-line stall

Содержание MUSE II

Страница 1: ...MAC PARA TECHNOLOGY LTD 1 máje 823 756 61 Rožnov pod Radhoštìm Czech Republic Tel 420 571 842 235 Tel fax 420 571 842 332 e mail mailbox macpara cz www macpara com USER MANUAL MUSE II MUSE II ...

Страница 2: ...raglider with maximum possible safety The MUSE II is constructed for thermal and cross country flying and will enable pilots to get maximum enjoyment Please read this manual carefully before you start this way you will get the most out of your glider and enjoy many Eden flights Paragliding is a sport which demands besides the optimum equipment a high degree of attentiveness good judgement and theo...

Страница 3: ...rim Safety equipment The is a second rib diagonal construction paraglider Every second main rib is attached to the lines and other ribs are attached at A B and C points thanks to the diagonal segments These segments do not lead to top surface of canopy but are attached at 80 of rib s height This technique was already used on the MUSE and is used by many other manufacturers in the industry The glid...

Страница 4: ...landing 6 Check whether the rescue system is correctly installed and secured 7 Inspection of the karabiner Inspection of the attachment and securing of the karabiner Find a suitable take off spot from which you can abort the take off at any point After checking the glider following the checklist lay it out with the cell openings upwards so that the canopy forms the shape of a horseshoe In a strong...

Страница 5: ...he brakes as abruptly as possible This dynamically increases the angle of attack and gives you the maximum braking effect Flight Steering Approach and landing MUSE II Turns with brakes Turns with brakes and weight shifting 8 Flight with speed system Towed and motorized flight To make faster flight possible the is equipped with a special speed system To accelerate the paraglider we recommend the fo...

Страница 6: ...e lines on the closed side If it is tangled pumping the brake line should help WARNING Take care to avoid applying too much brake when pumping out the deflation as this may disrupt the airflow over the canopy and lead to a stall Asymmetrical collapse Initiation MUSE II 10 WARNING In the case of a cravat which pumping of the brakes fails to release apply 50 70 brake on the open side of the canopy t...

Страница 7: ... canopy is caught in a cravat USE YOUR RESERVE Spin negative spirals Full stall Stalls Turbulence or rapid braking can lead to a pendulum effect and thus to changes in the angle of attack In extreme cases this can make the airflow break away from the upper surface of the canopy even without the brakes being activated Initiation Pull the brakes slowly down until you have no more forward speed The c...

Страница 8: ...II 14 Fly as far as possible from steep rises to give yourself space to lose height Sink rate approximately 3 5 m sec Sink rate approximately 4 6 m sec This allows rapid descent without stalling Sink rate depending on pilot 5 15 m sec Sink rate approximately 5 8 m sec End the stall with sufficient time for the airflow to re establish itself In principle always fly in such a way that you do not nee...

Страница 9: ...ad 80 kg Brake lines Dynema Polyester A 7850 100 Breaking Load 100 kg Main lines C1 C2 C3 D1 D2 D3 Aramid Polyester A 6843 160 Breaking Load 160 kgMain lines A1 A2 A3 B1 B2 B3 Aramid Polyester A 6843 240 Breaking Load 240 kg Wing tip line Aramid Polyester A 6843 080 Breaking Load 80 kg Main brake line Dynema Polyester A 7850 240 Breaking Load 240 kg STAP a s 407 80 VILEMOV CZECH REPUBLIC STAP POLY...

Страница 10: ...stC1 stD1 br1 br2 br3 br4 br5 br19 br20 br9 br11 br22 br21 mBR br23 br15 br17 br13 br6 br7 18 LINE PLAN BD B4 D4 B6 D6 mB1 mD1 B8 D8 br1 st0 stA2 stB2 stC2 stD2 stA1 stB1 stC1 stD1 br2 br3 br4 br5 br19 br20 br9 br11 br22 br21 mBR br23 br15 br17 br13 br6 br7 B10 D10 B16 D16 E16 Dt Dt Dt B12 D12 B18 D18 E18 mB2 mD2 mB3 mD3 B14 D14 B20 D20 E20 ...

Страница 11: ...or the A B arrays Replacements for damaged lines must be with new original lines Line lengths are taken from the lines data page Components of the check Porosity Overall strength check Line strength check MANUAL FOR PARAGLIDER CHECKS 20 Line length measurement Canopy line attachment points check Canopy fabric check Lines Connector check Risers Final check Lines should be separated and each line me...

Страница 12: ...3 26 71 29 18 Span flat m 10 31 10 91 11 55 11 95 12 5 Aspect ratio flat 4 65 4 65 4 65 4 65 4 66 Root cord m 2 7 2 85 3 02 3 12 3 27 Cells 39 39 39 39 39 Weight kg 5 2 5 45 5 95 6 45 6 95 Weight range kg 60 80 70 90 85 110 100 130 115 145 Min speed km h 22 24 22 24 22 24 22 24 22 24 Max speed km h 35 37 35 37 35 37 35 37 35 37 Top speed accelerator km h 45 46 45 46 45 46 45 46 45 46 Glide ratio 7...

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