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       Viper Jet Mk2
 
      
       
       
      The Viperjet Mk2 
      has been designed and developed with the use of computers and some of the 
      most advanced software available, by Airboss Aerospace, a engineering firm 
      located in Reno, NV.  The material used in the construction of the 
      Viperjet Mk2 is oven cured under 
      vacuumed carbon fibre with 1/2 inch honeycomb core. The aircraft has been 
      engineered to exceed FAA Part 23 Aerobatic Load Requirements. Also the 
      Viperjet Mk2has been designed 
      for easy construction and is only offered in a EXCEL Built configuration 
      with time saving subassemblies. Allowing the customer to complete their 
      project and spend more quality time flying and less time dreaming about 
      it.
 The astonishing performance of the Viperjet Mk2 demonstrates the outstanding skills of the design and 
      engineering team that collaborated to bring the aircraft to fruition. The 
      use of the best materials, the latest design techniques and construction 
      methods, together with rigorous quality control procedures, means that 
      Viper Aircraft Corporation is setting the foundation for a new standard in 
      the industry.
 
       With a choice of power plants from mild to wild the 
      Viperjet Mk2 can be tailored to 
      your distinctive taste. And wherever you are in the world you can always 
      be sure of Viper Aircraft support. The Viperjet Mk2 offers a remarkable turn of speed, and 
      performance without compromising safety. For example, the new
      aircraft delivers a estimated rate of climb 
      of well over 12,000 ft/min and speeds at altitude closing in on 500mph. 
      And with all of this performance the Viperjet Mk2 has a range of 800/1000nm range. Every attempt has 
      been made to give accurate information on performance, figures however 
      performance may vary depending on conditions. 
             
              
               | specifications 
 
              
                | powerplant propeller
 length
 height
 wing span
 wing area
 seats
 empty weight
 useful load
 gross weight
 fuel capacity
 range
 | x x
 24.8 ft.
 x
 25.83 ft.
 113.02 sq. ft.
 2
 2200 lbs.
 x
 3800 lbs.
 300 Gals.
 800-1000 s.m.
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            performance 
            
             
              
                | takeoff distance, 
                ground roll rate of climb
 max speed
 cruise speed
 landing distance, ground roll
 service ceiling
 | 1,200 ft. 10,000 - 12,000 
                fpm
 x
 450 kts
 2,000 ft.
 x
 |  
            limiting and recommended speeds
             
              
                | design manoeuvring speed (Va) never exceed speed (Vne)
 stall, power off (Vsl)
 landing approach speed
 | x x
 73 kts.
 x
 |  All specifications are based on manufacturer's 
            calculations
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