Размер

XXS

XS

S

M

L

XL

Удлинение

5,7

5,7

5,7

5,7

5,7

5,7

Размах, м

11,07

11,37

11,94

12,47

12,99

13,5

Площадь в проекции, кв. м.

18,12

19,13

21,06

23

24,94

26,94

Удлинение в проекции

4,1

4,1

4,1

4,1

4,1

4,1

Размах в проекции, м

8,61

8,85

9,3

9,71

10,11

10,51

Число секций

59

59

59

59

59

59

Высота стропления, м

6

6,17

6,48

6,77

7,05

7,33

Длина строп, м

240

245

257

269

280

291

Полётный вес, кг

55−75

60−80

75−95

85−105

95−115

105−135

Масса крыла, кг

4,4

4,6

5

5,4

5,8

6,3

Площадь**,м2

21,5

22,7

25

27,3

29,6

32

Центральная хорда, м

2,39

2,46

2,58

2,69

2,80

2,92

Ушная хорда, м

0,63

0,65

0,68

0,71

0,74

0,77

Масштабный коэф. %

0,93

0,953

1

1,045

1,088

1,131

Диаметры строп, мм

0.5/0.6/0.8/1.1/1.2/2.0

0.5/0.6/0.8/1.1/1.2/2.0

0.5/0.6/0.8/1.1/1.2/2.0

0.5/0.6/0.8/1.1/1.2/2.0

0.5/0.6/0.8/1.1/1.2/2.0

0.5/0.6/0.8/1.1/1.2/2.0

Производитель

Материал

Артикул

Верхняя поверхность (консоли, хвост)

NCV Industries / Dominico Tex

DOKDO-30DMF

9017(E25A)

Стропление, верхние ярусы

Rosenberger AG

Liros DC 60, DC 100

Стропление, нижние ярусы

Rosenberger AG

Liros PPSL 190 / PPSL 200 (L,XL)

Верхняя поверхность ( лоб)

NCV Industries / Dominico Tex

DOKDO-30DMF

9017(E25A)

Нервюры, косынки, крылья

NCV Industries / Dominico Tex

DOKDO-3MF

9017(E29A)

Управление, верхний, средний ярус

Rosenberger AG

Liros DC 40

Усиления петель

NCV Industries

2420

X15A

Петли строп

ОАО «Лента»

ЛТКП-15−185

Свободные концы

Güth & Wolf

Dyneema Core 70 404−15

Нитки (купол, стропы)

Amann Group

Nylon 46/2

Нитки (купол, свободные концы)

Amann Group

Nylon 69

Нижняя поверхность

NCV Industries / Dominico Tex

DOKDO-30DMF

9017(E25A)

Усиление передней кромки

Champion

Леска нейлон d=2мм

Manufacturer

Address

ParAAvis Co.

17A/2 st.lskry

Certification  number

Flight test

PG  1297.2018

31.01.2018

129344 Moscow

Russia

Glider model

Joy 3M

Classification

A

Serial number

J-5110

Representative

None

Trimmer

no

Place of test

Villeneuve

Folding lines used

no

Test pilot

Harness

Claude Thurnheer

Niviuk- Hamak M

Alain Zoller

Gin Gliders - Gingo 2 L

Harness to risers distance (em)

44

43

Distance between risers (em)

44

46

Total weight in flight (kg)

85

105

1.Inflation/Take-off

A

Rising behaviour

Smooth, easy and constant rising

A

Smooth, easy and constant rising

A

Specialtake off technique required

No

A

No

A

2.Landing

A

Speciallanding technique required

No

A

No

A

3.Speed in straight flight

A

Trim speed more than 30 km/h

Yes

A

Yes

A

Speed range using the controls larger than 10 kmlh

Yes

A

Yes

A

Minimum  speed

Less than 25 km/h

A

Less than 25 km/h

A

4.Control movement

A

Max. weight in flight up to 80 kg

Symmetric  controlpressure I travel

not available

0

not available

0

Max. weight in flight 80 kg to 100 kg

Symmetric  controlpressure I travel

Increasing I greater than 60 em

A

not available

0

Max. weight in flight greater than 100 kg

Symmetric  controlpressure I travel

not available

0

Increasing I greater than 65 em

A

5.Pitch stability exiting accelerated flight

A

Dive forward angle on exit

Dive forward less than 30°

A

Dive forward less than 30°

A

Collapse occurs

No

A

No

A

6.Pitch stability operating controls during accelerated flight

A

Collapse occurs

No

A

No

A

7.Roll stability and damping

A

Oscillations

Reducing

A

Reducing

A

8.Stability in gentle spirals

A

Tendency  to return to straight flight

Spontaneous exit

A

Spontaneous exit

A

9.Behaviour exiting a fully developed spiral dive

A

Initial response of glider (first 180°)

Immediate reduction of rate ofturn

A

Immediate reduction of rate ofturn

A

Tendency to return to straight flight

Spontaneous exit (g force decreasing, rate ofturn decreasing)

A

Spontaneous exit (g force decreasing, rate ofturn decreasing)

A

Turn angle to recover nonmal flight

Less than 720°, spontaneous

A

Less than 720°, spontaneous

A

recovery

recovery

10. Symmetric front collapse

A

Approximately 30 % chord

Rocking back less than 45°

A

Rocking back less than 45°

A

Recovery

Spontaneous in less than 3 s

A

Spontaneous in less than 3 s

A

Dive forward angle on exit Change of course

Dive forward oo to 30° Keeping course

A

Dive forward oo to 30° Keeping course

A

Cascade  occurs

No

A

No

A

Folding lines used

No

No

At least  50% chord

Entry

Rocking back less than 45°

A

Rocking back less than 45°

A

Recovery

Spontaneous in less than 3 s

A

Spontaneous in less than 3 s

A

Dive forward angle on exit I Change of course

Dive forward oo to 30° I Keeping

A

Dive forward oo to 30° I Keeping

A

course

course

Cascade  occurs

No

A

No

A

Folding lines used

No

No

With accelerator

Entry

Rocking back less than 45°

A

Rocking back less than 45°

A

Recovery

Spontaneous in less than 3 s

A

Spontaneous in less than 3 s

A

Dive forward angle on exit I Change of course

Dive forward oo to 30° I Keeping

A

Dive forward oo to 30° I Keeping

A

course

course

Cascade  occurs

No

A

No

A

Folding lines used

No

No

11. Exiting deep stall (parachutalstall)

A

Deep stall achieved

Yes

A

Yes

A

Recovery

Spontaneous in less than 3 s

A

Spontaneous in less than 3 s

A

Dive forward  angle on exit

Dive forward oo to 30°

A

Dive forward oo to 30°

A

Change of course

Changing course less than 45°

A

Changing course less than 45°

A

Cascade  occurs

No

A

No

A

12. High  angle  of attack  recovery

A

Recovery

Spontaneous in less than 3 s

A

Spontaneous in less than 3 s

A

Cascade  occurs

No

A

No

A

13. Recovery from a developed full stall

A

Dive forward  angle on exit

Dive forward oo to 30°

A

Dive forward oo to 30°

A

Collapse

No collapse

A

No collapse

A

Cascade occurs (other than collapses)

No

A

No

A

Rocking back

Less than 45°

A

Less than 45°

A

Line tension

Most lines tight

A

Most lines tight

A

14. Asymmetric collapse

A

Small asymmetric collapse

Change of course until re-inflation I Maximum dive forward or

Less than goo I Dive or roll angle

A

Less than goo I Dive or roll angle

A

roll angle

15oto 45o

oo to 15°

Re-inflation  behaviour

Spontaneous re-inflation

A

Spontaneous re-inflation

A

Total change of course

Less than 360°

A

Less than 360°

A

Collapse on the opposite side occurs

No (or only a small number  of

A

No (or only a small number  of

A

collapsed cells with a spontaneous

collapsed  cells with a spontaneous

reinflation)

reinflation)

Twist occurs

No

A

No

A

Cascade  occurs

No

A

No

A

Folding lines used

No

No

Large asymmetric collapse

Change of course until re-inflation I Maximum dive forward or

Less than goo I Dive or roll angle

A

Less than goo I Dive or roll angle

A

roll angle

15° to 45°

15° to 45°

Re-inflation  behaviour

Spontaneous re-inflation

A

Spontaneous re-inflation

A

Total change of course

Less than 360°

A

Less than 360°

A

Collapse on the opposite side occurs

No (or only a small number  of

A

No (or only a small number  of

A

collapsed cells with a spontaneous

collapsed  cells with a spontaneous

reinflation)

reinflation)

Twist occurs

No

A

No

A

Cascade  occurs

No

A

No

A

Folding lines used

No

No

Small asymmetric collapse with fully activated accelerator

Change of course until re-inflation I Maximum dive forward or roll angle

Less than goo I Dive or roll angle

15o to45o

A

Less than goo I Dive or roll angle oo to 15°

A

Re-inflation behaviour

Spontaneous re-inflation

A

Spontaneou s re-inflation

A

Total chan ge of course

Less than 360°

A

Less than 360°

A

Collapse on the opposite side occurs

No (or only a small number of collapsed cells with a spontaneous

A

No (or only a small number of collapsed cells with a spontaneous

A

reinflation)

reinflation)

Twist occurs

No

A

No

A

Cascade occurs

No

A

No

A

Folding lines used

No

No

Large asymmetric collapse  with fully  activated accelerator

Change of course until re-inflation I Maximum dive forward or roll angle

Less than goo I Dive or roll angle

15° to 45°

A

Less than goo I Dive or roll angle

15° to 45°

A

Re-inflation behaviour

Spontaneous re-inflation

A

Spontaneous re-inflation

A

Total change of course

Less than 360°

A

Less than 360°

A

Collapse on the opposite side occurs

No (or only a small number of

A

No (or only a small number of

A

collapsed cells with a spontaneous

collapsed cells with a spontaneous

reinflation)

reinflation)

Twist occurs

No

A

No

A

Cascade occurs

No

A

No

A

Folding lines used

No

No

15. Directionalcontrol with a maintained asymmetric

A

collapse

Able to keep course

Yes

A

Yes

A

180° tum away from the collapsed side possible in 10 s

Yes

A

Yes

A

Amount of control range between turn and stall or spin

More than 50 % of the symmetric

A

More than 50 % of the symmetric

A

controltravel

control travel

16. Trim speed spin tendency

A

Spin occurs

No

A

No

A

17. Low speed spin tendency

A

Spin occurs

No

A

No

A

18. Recovery from a developed spin

A

Spin rotation angle after release

Stops spinning in less than goo

A

Stops spinning in less than goo

A

Cascade occurs

No

A

No

A

19. B-llne stall

A

Change of course before release

Changing course less than 45°

A

Changing course less than 45°

A

Behaviour before release

Remains stable with straight span

A

Remains stable with straight span

A

Recovery

Spontaneous in less than 3 s

A

Spontaneous in less than 3 s

A

Dive forward angle on exit

Dive forward oo to 30°

A

Dive forward oo to 30°

A

Cascade occurs

No

A

No

A

20. Big ears

A

Entry procedure

Dedicated controls

A

Dedicated controls

A

Behaviour during big ears

Stable flight

A

Stable flight

A

Recovery

Spontaneous in less than 3 s

A

Spontaneous in less than 3 s

A

Dive forward angle on exit

Dive forward oo to 30°

A

Dive forward oo to 30°

A

21. Big ears in accelerated flight

A

Entry procedure

Dedicated controls

A

Dedicated controls

A

Behaviour during big ears

Stable flight

A

Stable flight

A

Recovery

Spontaneous in less than 3 s

A

Spontaneous in less than 3 s

A

Dive forward angle on exit

Dive forward oo to 30°

A

Dive forward oo to 30°

A

Behaviour immediately after releasing the accelerator while

Stable flight

A

Stable flight

A

maintaining big ears

22. Alternative means of directional control

A

180° turn achievable in 20 s

Yes

A

Yes

A

Stall or spin occurs

No

A

No

A

23. Any other flight procedure and/or configuration

0

described in the user's manual

Procedure works as described

not available

0

not available

0

Procedure suitable for novice pilots

not available

0

not available

0

Cascade occurs

not available

0

not available

0

24. Comments  oftest pilot