Technical Parameters

      BRISTELL LSA BRISTELL UL BRISTELL HD BRISTELL RG
Dimensions            
Wing span 9,13 m 8,13 m 8,13 m 9,13 m
Wing area 11,75 m2 10,5 m2 10,5 m2 11,75 m2
Wing loading 51,06 kg/m2 45 kg/m2 57,1 kg/m2 51,06 kg/m2
Aircraft length 6,45 m 6,45 m 6,45 m 6,45 m
Aircraft height 2,28 m 2,28 m 2,28 m 2,28 m
Cabin width 1,3 m 1,3 m 1,3 m 1,3 m
Weights            
Empty weight 320 kg 290 kg 310 kg 330 kg
Maximum take-off weight 600 kg 472,5 kg 600 kg 600 kg
Useful  load 280 kg 182,5 kg 290 kg 270 kg
Fuel tanks capacity 120 l 120 l 120 l 120 l
Load factors +4/-2g
Operational speeds            
Stall speed with flaps VSO 62 km/h 63 km/h 65 km/h 62 km/h
Stall speed without flaps VS1 80 km/h 80 km/h 82 km/h 80 km/h
  Manoeuvring speed VA 180 km/h 166 km/h 180 km/h 180 km/h
Maximum flap speed VF 139 km/h
Cruising speed VC 250 km/h 214 km/h 250 km/h 250 km/h
Never exceeded speed VNE 290 km/h 270 km/h 290 km/h 290 km/h
Power units            
ROTAX 912 UL 80 Hp
ROTAX 912 ULS 100 Hp
ROTAX 912 iS 100 Hp