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7

 strong, take some of the pressure out of the canopy by taking in one or both of the brake-
lines (or the C-risers).

Always fly with sufficient clearance from the terrain. The 

 glides best with open 

brakes, descends best with lightly applied brakes. In turbulence fly with brakes lightly 
applied to avoid canopy collapse. If the canopy pendulums forward, this should be 
corrected by prompt braking. A pendulum movement of the canopy backwards is 
corrected by loosening the brakes in good time.

Turns can be initiated using the brakes in two different ways.

The pilot pulls the brake on the side to which he wishes to turn. To minimise sinking, the 
brake on the outside of the curve is lightly applied.

The pilot pulls the brake on the side to which he wishes to turn and shift his weight to the 
same side. Turns can also be flown with the harness alone, by shifting the weight to the 
inside of the curve. This weight shift has a greater effect, the more loosely the chest-strap 
is fastened. An optimal steering technique is achieved by a combination of braking and 
weight shifts. It is pilot's skill to use both of these techniques specially in thermals.

A further possibility for steering is best limited to emergencies (if the brake-lines break, for 
example). This entails gently pulling the front (watch out for collapse of the canopy) or on 
D-riser (beware asymmetrical stall). We recommend that you do not use this form of 
steering in normal flight.

To avoid stressful situations in the approach to landing, it is important to initiate the 
process at an adequate altitude. This leaves you enough time to observe and 
appropriately deal with wind direction and any other aircraft in your vicinity.

The final approach should generally be made into the wind and with fully released 
brakes, in order to maintain maximum energy in the glider. If the air is turbulent, it is better 
to land lightly braked to minimise the possibility of the canopy collapsing. In order to land 
on your feet, rather than lying on your back, you will need to lean forward in the harness 
not lower than 5 m above the ground. At an adequate height (about 1-2 m above the 
ground), pull both brakes fully down until the glider is sufficiently slowed.

In a light headwind pulling the brakes only lightly is enough to give a soft landing. In a 
calm, or even tailwind, you must pull the 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 following steps:
     a) extend the speed bar
     b) use the speed bar to control speed

Never activate the speed system in turbulence, at low altitude, or when approaching a 
landing (the lower angle of attack results in less stability despite the higher speed).

The 

 is suitable for towed flight, and is excellent glider for flying   with a paramotor!

 has no tendencies towards deep stall/parachuting. Therefore we allow tow- 

launched flights with a similar techniques to that described above. There is sufficient 
margin to countersteer the glider in a normal towing situation. Make sure you use proper 
equipment, experienced personnel and all relevant safety precautions for towing.

This section describes flying conditions which can be deliberately induced, or which can 
develop unintentionally due to turbulence or pilot error. Any pilot who flies through 
turbulence is sure to be faced with these special flight conditions at some point. So take a 
good look at these flight manoeuvres or prepare for them by SIV (safety training over 
water). Mastering these flying conditions significantly improves your active flight safety. 
Sufficient height, as well as the carrying of a reserve parachute, is imperative.

MUSE II

MUSE II

MUSE II

Note!! 

However, motorized flying has been made with great success due to its very easy 

take-off characteristics, stability and good handling, always use certified combinations 
of engine - harness - glider. If in doubt check with your federation.

WARNING!!

 Please always ensure that the brake lines are adjusted to the lengths 

recommended here. Setting them shorter could lead to a tendency to stall during towed 
flight. Apart from this, there are no special procedures.

WARNING!!

 The MUSE II is not suitable for jumps from aircraft.

WARNING!!

 All the critical flight conditions described here require thorough knowledge; 

otherwise carrying them out may be very dangerous. Sufficient height above the ground 
is imperative. Bear in mind that all disturbances of the canopy can increase the sink rate 
by 2 - 10 m/sec, depending on the degree of disturbance. Carrying out these 
manoeuvres wrongly may lead to a crash.

EXTREME AND CRITICAL FLIGHT MANOEUVRES

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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