
            
      On June 1, 1974, the KR-2, a two seat version emerged into 
      the world of experimental aviation with its maiden flight. The prototype 
      KR-2, N4KR, was powered by an 1834cc Revmaster, which is an otherwise 
      stock 1600cc VW with 99mm cylinders. This particular engine was a single 
      ignition version and used a Bendix mag and a Posa carburettor. Revmaster 
      gives the engine a continuous rating of 60 hp at 3000 rpms, which is on 
      the conservative side. Ken Rand, the designer/builder, obtained cruise 
      speeds of 180mph at 3200 rpm and airspeeds of 200mph at higher altitudes. 
      Some aircraft have not been built sufficiently lightweight and became in 
      effect single seaters.
            
      A KR2 fitted with a Jabiru engine (lighter with more power) 
      has flown from the UK to Australia and back with 2 people.
            
             
              
               
               
               specifications 
 
              
                
                powerplant 
                propeller 
                length 
                height 
                wing span 
                wing area 
                seats 
                empty weight 
                
                useful load 
                gross weight 
                fuel capacity 
                range | 
                
                VW 2100 
                x 
                
            14' 6" 
                
                x 
                
            20' 8" 
                
            80 sq. ft. 
                
            420 lbs. 
                
            480 lbs. 
                x 
                
            900 lbs. 
                35 gal 
                
                1600 miles | 
               
             
            
            performance 
            
             
            
              
                
                takeoff distance, 
                ground roll 
                rate of climb 
                max speed 
                cruise speed 
                landing distance, ground roll 
                
                
                service ceiling | 
                
                350 ft. 
                800 fpm 
                
                200 mph 
                
                180 mph 
                
            900 ft. 
                
                15,000 ft. | 
               
             
            
            limiting and recommended speeds
             
            
              
                
                design manoeuvring speed (Va) 
                never exceed speed (Vne) 
                stall, power off (Vsl) 
                landing approach speed  | 
                
                
                x 
                x 
                
                52 mph 
                x | 
               
             
            All specifications are based on manufacturer's 
            calculations 
            Fixed conventional or trigear, or retractable 
            conventional 
   |