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       Glasair 
      1
 
      
       
             
            The Glasair was the first kit aircraft that used 
            moulded surfaces rather than the Rutan method of construction. The 
            original Glasair 1 required a very long time to construct. The original company, Stoddard 
            Hamilton, (named after the late designer) went into liquidation due 
            to reasons outside the Glasair range. Fortunately the company was 
            purchased by aircraft enthusiast 
            Thomas W. Wathen and is now going from 
            strength to strength. The Glasair range included a taildragger 
            version (TD), fixed trike (FT) and a retract (RG). Wing extensions 
            were available which improved performance at higher altitude but 
            reduced g loadings. 
            The Glasair is the ideal long distance fast personal 
            aircraft. 
            These aircraft are not only extremely strong, but fly 
            better than almost any experimental. They are renowned for their 
            handling characteristics. In addition, the resins used very rarely 
            cause allergy problems for builders.  
            Performance is varied according to choice of engine, which can range 
            from 160 hp to 200 hp.  
             
            specifications and performance figures for 200 hp variant with 
            extended fuel tanks and no wing extensions 
             
              
               | specifications (RG) 
 
              
                | powerplant propeller
 length
 height
 wing span
 wing area
 seats
 empty weight
 useful load
 gross weight
 fuel capacity
 range
 | Lyc IO 360 A1B 200 hp 3 blade Hoffmann VP wood blades
 19ft 6ins
 6ft 2 ins
 24ft 4ins
 81.3 sq ft
 2
 1368lbs
 632lbs
 2000lbs  
                
                (In USA 
        2200lbs allowable)
 61.4 Imp gal.
 1177 
         Miles
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            performance 
            
             
              
                | takeoff distance, 
                ground roll rate of climb
 max speed
 cruise speed
 landing distance, ground roll
 service ceiling
 | 400m 1500 ft/min
 260 
         mph
 175 kts 
         IAS
 500m
 19,000ft
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            limiting and recommended speeds
             
              
                | design manoeuvring speed (Va) never exceed speed (Vne)
 stall, power off (Vsl)
 landing approach speed
 | 145  mph 260  mph
 65 mph
 90  mph
 |  All specifications are based on manufacturer's 
            calculations
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