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Technical details
IOTA 2
Flat surface
Projected surface
Ideal weight range * **
Certified takeoff weight **
Glider weight
Aspect ratio
Projected aspect ratio
Flat span
Projected span
Certification
Number of cells
Number of risers
Maximum chord
Max lenght of the risers
Accelerator tavel max .
Max length of the lines with the risers
Trims
Max . sym . brake travel at max . weight
Other adjustable / removable /
variable devices
*
Takeoff weight range in which the IOTA 2 shows the best relationship between flying speed and climb
* ** Pilot, wing, equipment
21
23
m
21 .8
23 .7
2
m
18 .8
20 .4
2
kg
65–75
75–85
kg
60–77
70–88
kg
4 .30
4 .60
5 .6
5 .6
4 .23
4 .23
m
11 . 1
11 .5
m
8 .9
9 .3
EN/LTF-B
EN/LTF-B
59
59
3+1
3+1
m
2 .42
2 .53
cm
47
47
cm
10
13
m
6 .85
7 . 1 5
–
–
cm
73
76
–
–
25
27
25 .7
27 .7
22 .2
23 .9
85–97
97–110
80–100
92–114
4 .85
5 . 1 5
5 .6
5 .6
4 .23
4 .23
12 .0
12 .5
9 .7
10 .0
EN/LTF-B
EN/LTF-B
59
59
3+1
3+1
2 .63
2 .73
49
51
14
15
7 .45
7 .73
–
–
77
78
–
–
29
29 .7
25 .6
110–125
105–128
5 .40
5 .6
4 .23
12 .9
10 .4
EN/LTF-B
59
3+1
2 .83
53
15 .5
8 .00
–
79
–
35
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