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                  Mini Imp 
      
      
        
        
                    
              During the energy crisis of the mid 1970’s Moulton 
              B. (Molt) Taylor , designer of the certified Aerocar, the Coot 
              Amphibian, the IMP, and many other aircraft for the US Navy during 
              W.W.II, decided to turn his many talents to a small, 
              easy-to-build, light plane which focused on maximum cruise speed 
              and efficiency. The result is the Taylor Mini-IMP. 
              The Mini-IMP is a “second 
              generation” version of the original, 2+2 place, Taylor IMP (an 
              acronym for Independently Made 
              Plane) 
              homebuilt aircraft. This original version proved to be too 
              complicated and too costly to build for the “average” homebuilder. 
              Accordingly, since the IMP offered great opportunity for further 
              simplification, and had the potential of giving performance equal 
              to or better than some of the other “mini” designs being offered 
              at the time, it was decided to scale the IMP configuration down to 
              a single-place design, to design it to accommodate a great variety 
              of engines, and to further simplify it’s construction. The 
              Mini-IMP was the result. 
              
              The Mini-IMP Aircraft Company has been formed to keep the aircraft design available, to provide 
              builder support and to further promote this interesting aircraft 
              design. 
            
             
              
               
               
               specifications 
 
              
                
                powerplant 
                propeller 
                length 
                height 
                wing span 
                wing area 
                seats 
                empty weight 
                
                useful load 
                gross weight 
                fuel capacity 
                range | 
                
                
                Continental O-200, 100 hp (75 kW) 
                 
                x 
                
        
                24 ft 6 in  
                
        4 ft 0 in 
                
        17 ft 0 in 
                
                x 
                1 
                
        780 lb 
                x 
                
        1,000 lb 
                
                x 
                
        500 miles | 
               
             
            
            performance 
            
             
            
              
                
                takeoff distance, 
                ground roll 
                rate of climb 
                max speed 
                cruise speed 
                landing distance, ground roll 
                
                
                service ceiling | 
                
                x 
                
        1,500 ft/min 
                
        200 mph 
                x 
                x 
                x | 
               
             
            
            limiting and recommended speeds
             
            
              
                
                design manoeuvring speed (Va) 
                never exceed speed (Vne) 
                stall, power off (Vsl) 
                landing approach speed  | 
                
                
                x 
                x 
                x 
                x | 
               
             
            All specifications are based on manufacturer's 
            calculations 
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