The new project (Aero-service companies): Ultralight Aeroplane PUMA

Projected deadline flight first copy April 2009


The parameters aircraft:

• Length 6.5 m
  
  
• As 9.1 m
  
  
• Area sash 11.3 m2
  
  
• A wing trapezoidal converge having twisted aerodynamic and geometric 2.5 degree
  
  
• Mass of empty aircraft ready to fly 295 kg
  
  
• Maximum-off weight of 472.5 kilograms rescue system
  
  
• Capacity fuel tank 50 + 50 = 100 l
  
  
• Engine R912, R912S, R914, BMW 1100
  
  
• Under the power-reared
  
  
• The diameter of 360 mm chassis wheels
  
  
• The rules according to which it is proposed UL-2, JAR-VLA
  
  
• Maximum limit overload +4 / -2
  
  
• Speed dragging without flaps of 77 km / h
  
  
• Speed dragging BONNETS at 61 km / h
  
  
• Cruising speed (Travel) 240 km / h
  
  
• Speed maximum in horizontal flight 265 km / h
  
  
• Can not speed to 300 km / h