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150 00 Praha 5 - Motol
Czech Republic
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Technical Data

Nevada light

Units


22

24

26

28

Flat area

[m2]


21,76

23,68

25,79

28,1

Projected area

[m2]


18,83

20,49

22,31

24,31

Span

[m]


11,1

11,58

12,08

12,61

Projected span

[m]


8,99

9,38

9,79

10,22

Aspect ratio



5,66

5,66

5,66

5,66

Projected aspect ratio



4,29

4,29

4,29

4,29

Max. chord

[m]


2,48

2,59

2,7

2,82

Min. chord

[m]


0,54

0,56

0,59

0,62

Number of cells



56

56

56

56

Line consumption

[m]


211,3

220,6

230,2

240,3

Weight of the glider

[kg]


3,4

3,8

4,2

4,6

Take-off weight range

[kg]


62 – 77

75 - 90

85 - 100

95 - 115

Certification EN/LTF



B

B

B

B

Basic speed*

km/h


38

38

38

38

Max. speed*

km/h


55+

55+

55+

55+

Min. sink rate*

m/s


1.0

1.0

1.0

1.0

Glide ratio*



9,5+

9,5+

9,5+

9,5+

These data are valid at the mid-point of weight range. 


Note: performance data are dependant upon the wing loading, type of harness and position of the pilot