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Tecma Nuage
 
Tecma-Nuage
 
First built in 1987, the Nuage was for intermediate pilots.
 
A 135 model with smaller A frame (uprights 1.50m) was available.
 
The manufacturer proposes a modification: move the position of the trapese on the keel + change of the cables + reinforcement on the keel to improve the thrust to the attero. This reduces the tendency to plant the nose with the landing.
 
Nuage 135
Wing area: 13.5 m²
Wing span: 9.6 m
Aspect ratio: 6.7
Hang glider weight: 24 kg
Minimum pilot weight: 58 kg
Maximum pilot weight: 68 kg
Packed length short: 3.4 m
Nose angle: 124°
 
Nuage 150
Wing area: 15 m²
Wing span: 10 m
Aspect ratio: 6.7
Hang glider weight: 28 kg
Minimum pilot weight: 65 kg
Maximum pilot weight: 80 kg
Max speed: 80 kph
No of battons: 17
Packed length short: 3.6 m
Nose angle: 124°
 
Nuage 155
Wing area: 16 m²
Wing span: 10.4 m
Aspect ratio: 6.7
Hang glider weight: 30 kg
Minimum pilot weight: 68 kg
Maximum pilot weight: 90 kg
Packed length short: 4 m
Nose angle: 124°
 
Nuage 160
Wing area: 16 m²
Wing span: 10.4 m
Aspect ratio: 6.7
Hang glider weight: 32 kg
Minimum pilot weight: 85 kg
Maximum pilot weight: 100 kg
Packed length short: 4.2 m
Nose angle: 124°
 
 
 
 


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