| My Part 103 compliant ultralight self-launching sailplane.
                                    
                                    The large pictures show the project as it was in August 2010. It was to a point where it was ready for more test flying after
                                    some refinements were made.
                                     
                                      
                                    The Red Tail Hawk has a laminar flow airfoil, a carbon fiber tail boom and tail surfaces, welded steel tube frame, fiberglass
                                    shell.
                                     
                                      
                                    It is launched with a battery powered electric motor, spinning a folding propeller, that is shut down once enough altitude
                                    is reached for soaring like a conventional sailplane.
                                     
                                    
                                    
                                      
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                                    I have have a blog where I write about the design and construction of the Red Tail Hawk in detail. And also consider the issues
                                    of a version that others could build. It is a Yahoo email group, and allows some feed back from readers, but is operated mostly
                                    as a blog. You will need to join the group to read and post comments.
                                    
                                 
                                 
                                  Link to my Red Tail Hawk blog:
                                  
 
 Here is a video of a static run-up of the e-power system on the Red Tail Hawk, done in early June, 2009.
 
                                    click here to play video
                                    
                                  
 
                                     
                                       
                                          
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                                             | Proof-loading a nose sample, over 6 g with no distortion |  
                                     
                                       
                                          
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                                             | Foam and fiberglass nose, aluminum aft of spar | 
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