Main Menu

Aerotecknik CZ Sro VUT-100 Cobra

 

vut100cobra


Initial work on the VUT100 Cobra project began in 2001 with the maiden flight made in November 2004. October 2006 saw the maiden flight of the VUT100 SuperCobra.


The VUT 100 Cobra was designed to offer speed with cabin comfort and ergonomics, low cost of ownership and long range. Planned to be available in two versions differing by the power units: The VUT 100-120i is equipped with a Lycoming IO-360-A1B6 (200HP) and mt-propeller MTW-12. The VUT 100-131i is equipped with a Lycoming IO-580-B1A (315HP) and the mt-propeller MTV-9.


The VUT100 Cobra was designed to enable easy and fast access to the parts of the airframe which require inspections and maintenance and the number of nodes which require inspections and adjustment were minimized.


The development team designed the airframe from traditional duralumin using 3D design systems and optimized from the strength point of view by FEM methods.

 

VUT100-120i
Engine: Lycoming IO-360-A1B6, 200 hp    
Propeller: Hartzell HC-F3YR-1RF
Diameter: 74 in / 188 cm            
Type: 3 blade, constant speed
Length: 26.3 ft / 8 m            
Wing span: 33.5 ft / 10.2 m
Internal cabin length: 122 in / 3.1 m            
Seats: 4
Internal cabin width: 51.5 in / 1.31 m             
Fuel usable: 90 USG / 340 lt
Internal cabin height: 48 in / 1.22 m            
Max. take-off: 2,930 lb / 1,330 kg
Useful load: 1,105 lb / 500 kg            
Max. level speed: 155 kts / 287 km/h
Max. rate of climb: 1,000 fpm / 5 m/s            
Stall speed: 50 kts / 93 kph
Range: 1,080 nm / 2,000 km        
Endurance: 8 hrs
Load factors: +3.8g -1.52g (Normal category) / +4.4g -1.76g (Utility category)

VUT100-131i
Engine: Lycoming IO-580-B1A, 315 hp    
Propeller: Hartzell HC-F3YR-1RF
Diameter: 76 in / 193 cm            
Type: 3 blade, constant speed
Length: 26.3 ft / 8 m            
Wing span: 33.5 ft / 10.2 m
Internal cabin length: 122 in / 3.1 m             
Seats: 4
Internal cabin width: 51.5 in / 1.31 m             
Fuel usable: 90 USG / 340 lt
Internal cabin height: 48 in / 1.22 m            
Max. take-off: 3,200 lb / 1,450 kg
Useful load: 1,260 lb / 570 kg            
Max. level speed: 175 kts / 324 km/h
Max. rate of climb: 1,000 fpm / 5 m/s            
Stall speed: 55 kts / 103 km
Range: 1,000 nm / 1,830 km        
Endurance: 6 hrs
Load factors: +3.8g -1.52g (Normal category) / +4.4g -1.76g (Utility category)

 

 


Copyright © 2017 all-aero. All Rights Reserved.
Joomla! is Free Software released under the GNU General Public License.