Yang 28
Paraglider circa 1998.
Wing area: 28.6 sq.m
Pilot weight: 65-85 kg
No. of cells: 32
Wing span: 9.8 m
Aspect ratio: 3.4
Min sink: 1.3 m/s
Max speed: 38 kph
Yang 31
Paraglider circa 1998.
Wing area: 31 sq.m
Pilot weight: 85-105 kg
No. of cells: 34
Wing span: 10.6 m
Aspect ratio: 3.6
Min sink: 1.3 m/s
Max speed: 38 kph
Quix 26
Paraglider circa 1998.
Wing area: 26.43 sq.m
Pilot weight: 60-80 kg
No. of cells: 45
Wing span: 11.11 m
Aspect ratio: 4.67
Min sink: 1.1 m/s
Max speed: 45 kph
Quix 28
Paraglider circa 1998.
Wing area: 28 sq.m
Pilot weight: 80-95 kg
No. of cells: 45
Wing span: 11.83 m
Aspect ratio: 4.9
Min sink: 1.1 m/s
Max speed: 45 kph
Quix 31
Paraglider circa 1998.
Wing area: 31 sq.m
Pilot weight: 95-110 kg
No. of cells: 51
Wing span: 12.34 m
Aspect ratio: 4.9
Min sink: 1.1 m/s
Max speed: 45 kph
Maxi BI
Paraglider circa 1998.
Wing area: 42.3 sq.m
Pilot weight: 130-210 kg
No. of cells: 49
Wing span: 14 m
Aspect ratio: 4.6
Min sink: 1.3 m/s
Max speed: 50 kph
Divine 26R
Paraglider circa 1998.
Wing area: 26.47 sq.m
Pilot weight: 75-95 kg
No. of cells: 75
Wing span: 12.74 m
Aspect ratio: 6.13
Min sink: 0.9 m/s
Max speed: 63 kph
Divine 27
Paraglider circa 1998.
Wing area: 27.47 sq.m
Pilot weight: 75-90 kg
No. of cells: 63
Wing span: 12.13 m
Aspect ratio: 5.3
Min sink: 1 m/s
Max speed: 50 kph
Divine 29
Paraglider circa 1998.
Wing area: 29.2 sq.m
Pilot weight: 90-105 kg
No. of cells: 66
Wing span: 12.73 m
Aspect ratio: 5.55
Min sink: 1 m/s
Max speed: 50 kph
Divine 31
Paraglider circa 1998.
Wing area: 30.93 sq.m
Pilot weight: 105-120 kg
No. of cells: 69
Wing span: 13.33 m
Aspect ratio: 5.74
Min sink: 1 m/s
Max speed: 50 kph
Fancy 28
Paraglider circa 1998.
Wing area: 28 sq.m
Pilot weight: 65-85 kg
No. of cells: 44
Wing span: 11.15 m
Aspect ratio: 4.45
Min sink: 1.2 m/s
Max speed: 40 kph
Fancy 30
Paraglider circa 1998.
Wing area: 29.6 sq.m
Pilot weight: 80-100 kg
No. of cells: 40
Wing span: 11.68 m
Aspect ratio: 4.61
Min sink: 1.2 m/s
Max speed: 40 kph
With a chassis designed to work in extreme conditions and on professional jobs, there are 2 sizes: 1450 and 1400. Both have 200 cc power with Carbon Tripal propellers (recommended 130cm).
The engine can fly 4-5 hours and then carry out two seater flights.
The chassis can be dismantled into 4 stainless steel parts, or on request at 2, 3, or 5 parts. They are TIG welded, using stainless steel pipes, 304 & 316 grade in 6, 8, 10, 12 and 16 mm in the central part of the chassis frame. The 16 mm tube offers a double impact resistance.
There were more than 15 models of chassis, to mount any engine or incorporate the Evolution & Fly 100 EVO range of light engines,
Price 2009: US$1,650
F 200 1400
Engine: F 200, 200 cc
Carburettor: Walbro 37
Power: 27 hp
Belt reduction: 1 / 3
Cooling: Air
Clutch: No
Thrust: 78 kg
Fuel: 98 Green
Fuel tank: 14 lt
Consumption: 3 lt/hr
Frame dimensions: 130 x 130 x 27 cm
Prop: BA014 – Wood 125 or BA015 – 3 parts, Carbon 120 cm
Weight: 30 kg
Max pilot weight: 120 kg
Recomended pilot weight: 100 kg
Harness: Freedom
Parachute container: Down System
Parachutes sling: Serial
F 200 1450
Engine: F 200, 200 cc
Carburettor: Walbro 37
Power: 27 hp
Belt reduction: 1 / 3
Cooling: Air
Clutch: No
Thrust: 82 kg
Fuel: 98 Green
Fuel tank: 14 lt
Consumption: 3 lt/hr
Frame dimensions: 140 x 140 x 27 cm
Prop: BA016 – 3 parts, Carbon 130 cm
Weight: 31.5 kg
Max pilot weight: 200 kg+ Tandem
Recomended pilot weight: 125+ kg
Harness: Freedom
Parachute container: Down System
Parachutes sling: Serial
The first generation of the DHV 1-2 Atis glider was voted as the glider of a year by VOL LIBRE. The Atis 2 has new certification EN-B based on CEN 926-1 and 926-2, new profile, new layout and new experience.
(EN B equals the DHV 1-2 classification of the glider, the certification is different, and CEN 926-2 is different from DHV certification!)
The main changes compared to the first generation of the glider:
New profile with lighter ribs concept and higher speed range
New layout scheme
New design of stabilizers
Higher speed range with lower sink and higher glide efficiency
New, easy to use and highly efficient speed system
New geometry
New technology of the leading edge design
Trailing edge with velcro opening for easy cleaning of the canopy
Atis 2 (DHV 1-2) Price 2009: US$3,500.00
The Sky Paragliders Atis Acro model intended for Acro pilots is based in Sky’s intermediate glider, the Atis, released in 2002 in 3 sizes and about to have certification for the 4th, an XS (DHV 1-2). The Atis Acro had a good debut in the hands of pilot Tomas Lednik, who took the 3rd place at the past Oludeniz Air Games in Turkey with it. It is a small glider (XS size) and favoured with more speed and dynamic response than the serial model, thanks to a different plan layout.
ATIS 2SMLXL
Layout surface: 23,11 sq.m
Layout span: 10,86 m
Layout aspect ratio: 5,10
Projected surface: 20,69 sq.m
Projected span: 9,10 m
Projected aspect ratio: 4,00
Number of cells: 53
Weight of the glider: 5,0 kg
Take-off load: 60-80 kg
Trim speed: 37 km/h
Minimum speed: 23 km/h
Maximum speed: 48 km/h
Max. gliding ratio: 8,5
Min. sink rate: 1,15 m/s
Test: EN B
ATIS 2SMLXL
Layout surface: 25,00 sq.m
Layout span: 11,29 m
Layout aspect ratio: 5,10
Projected surface: 22,38 sq.m
Projected span: 9,47 m
Projected aspect ratio: 4,00
Number of cells: 53
Weight of the glider: 5,2 kg
Take-off load: 75-95 kg
Trim speed: 37 km/h
Minimum speed: 23 km/h
Maximum speed: 48 km/h
Max. gliding ratio: 8,5
Min. sink rate: 1,15 m/s
Test: EN B
ATIS 2SMLXL
Layout surface: 26,65 sq.m
Layout span: 11,66 m
Layout aspect ratio: 5,10
Projected surface: 23,86 sq.m
Projected span: 9,77 m
Projected aspect ratio: 4,00
Number of cells: 53
Weight of the glider: 5,4 kg
Take-off load: 87-110 kg
Trim speed: 37 km/h
Minimum speed: 23 km/h
Maximum speed: 48 km/h
Max. gliding ratio: 8,5
Min. sink rate: 1,15 m/s
Test: EN B
ATIS 2SMLXL
Layout surface: 28,83 sq.m
Layout span: 12,12 m
Layout aspect ratio: 5,10
Projected surface: 25,80 sq.m
Projected span: 10,16 m
Projected aspect ratio: 4,00
Number of cells: 53
Weight of the glider: 5,7 kg
Take-off load: 105-130 kg
Trim speed: 37 km/h
Minimum speed: 23 km/h
Maximum speed: 48 km/h
Max. gliding ratio: 8,5
Min. sink rate: 1,15 m/s
Test: EN B
Fides 2 is a school glider certified in the DHV 1 category. The Fides 2 is excellent for first XC flights and was the lightest glider – in the category – produced with the standard materials in the market. Price 2009: US$3,000.00
Fides 2XS
Layout surface: 22,36 sq.m
Projected surface: 19,65 sq.m
Layout span: 10,25 m
Projected span: 8,24 m
Layout aspect ratio: 4,70
Projected aspect ratio: 3,46
Take-off weight: 56-74 kg
Weight of the glider: 4,2 kg
Min. speed: 22 km/h
Trim speed: 36 km/h
Max. speed: 45 km/h
Sinkrate: <1,2 m/s Gliding ratio: >7,5
Certification: AFNOR Standard
Fides 2 S
Layout surface: 24,19 sq.m
Projected surface: 21,26 sq.m
Layout span: 10,66 m
Projected span: 8,57 m
Layout aspect ratio: 4,70
Projected aspect ratio: 3,46
Take-off weight: 69-90 kg
Weight of the glider: 4,5 kg
Min. speed: 22 km/h
Trim speed: 36 km/h
Max. speed: 45 km/h
Sinkrate: <1,2 m/s Gliding ratio: >7,5
Certification: DHV 1
Fides 2XSSML
Layout surface: 22,36 sq.m
Projected surface: 19,65 sq.m
Layout span: 10,25 m
Projected span: 8,24 m
Layout aspect ratio: 4,70
Projected aspect ratio: 3,46
Take-off weight: 56-74 kg
Weight of the glider: 4,2 kg
Min. speed: 22 km/h
Trim speed: 36 km/h
Max. speed: 45 km/h
Sinkrate: <1,2 Gliding ratio: >7,5
Certification: AFNOR Standard
Fides 2XSSML
Layout surface: 24,19 sq.m
Projected surface: 21,26 sq.m
Layout span: 10,66 m
Projected span: 8,57 m
Layout aspect ratio: 4,70
Projected aspect ratio: 3,46
Take-off weight: 69-90 kg
Weight of the glider: 4,5 kg
Min. speed: 22 km/h
Trim speed: 36 km/h
Max. speed: 45 km/h
Sinkrate: <1,2 Gliding ratio: >7,5
Certification: DHV 1
Fides 2XSSML
Layout surface: 26,17 sq.m
Projected surface: 23,00 sq.m
Layout span: 11,09 m
Projected span: 8,92 m
Layout aspect ratio: 4,70
Projected aspect ratio: 3,46
Take-off weight: 82-105 kg
Weight of the glider: 4,8 kg
Min. speed: 22 km/h
Trim speed: 36 km/h
Max. speed: 45 km/h
Sinkrate: <1,2 Gliding ratio: >7,5
Certification: DHV 1
Fides 2XSSML
Layout surface: 28,30 sq.m
Projected surface: 24,87 sq.m
Layout span: 11,54 m
Projected span: 9,28 m
Layout aspect ratio: 4,70
Projected aspect ratio: 3,46
Take-off weight: 100-130 kg
Weight of the glider: 5,1 kg
Min. speed: 22 km/h
Trim speed: 36 km/h
Max. speed: 45 km/h
Sinkrate: <1,2 Gliding ratio: >7,5
Certification: DHV 1
Fides 2M
Layout surface: 26,17 sq.m
Projected surface: 23,00 sq.m
Layout span: 11,09 m
Projected span: 8,92 m
Layout aspect ratio: 4,70
Projected aspect ratio: 3,46
Take-off weight: 82-105 kg
Weight of the glider: 4,8 kg
Min. speed: 22 km/h
Trim speed: 36 km/h
Max. speed: 45 km/h
Sinkrate: <1,2 m/s Gliding ratio: >7,5
Certification: DHV 1
Fides 2L
Layout surface: 28,30 sq.m
Projected surface: 24,87 sq.m
Layout span: 11,54 m
Projected span: 9,28 m
Layout aspect ratio: 4,70
Projected aspect ratio: 3,46
Take-off weight: 100-130 kg
Weight of the glider: 5,1 kg
Min. speed: 22 km/h
Trim speed: 36 km/h
Max. speed: 45 km/h
Sinkrate: <1,2 m/s Gliding ratio: >7,5
Certification: DHV 1
1998: Kamenec 388, CZ-73911 Frydlant, Czech Republic
After the excellent Divine, a good compromise between performance and safety, the tide then turned for the company with the death of the designer at the PWC in Spain.
Originally designed in Slovenia, the make was the exported to the Czech Republic for the better production facilities there.
The Sky Motors 70 four-cylinder inline air-cooled aero engine produced 60hp from 200ci and received ATC 200.
The 70A was a model 70 with modified crankcase and crankshaft.
