Difference between revisions of "3D Printed Aerodynamic Parts"

Jump to navigation Jump to search
m
fix image
(Created page with " -Nose Cones -Fin Cans")
 
m (fix image)
 
(9 intermediate revisions by 3 users not shown)
Line 1: Line 1:
[[File:3D_Printed_Cigar_Rocket.jpg|thumb]]
For [[User:holmaschine|holmaschine]], the advantage of 3-D printed model rocket parts is the ability to create a very thin and structurally efficient shape without concern over fabrication and the relative alignments of subparts.  Components can be printed true to final form (+/-) with only light treatment required to smooth outer surfaces so long as the basic restrictions of the manufacturing method are understood.


-Nose Cones




-Fin Cans
'''Nose Cones'''
 
Several prototypes have been created in both 29mm and 65mm diameter, using a tangent-ogive profile.
 
 
TO DO: write code to generate g-code directly instead of using SolidWorks and Slic3r.
 
WHY: avoid 15 min + delay time using slicer, better match to theoretical shape without.
 
 
TO DO: Model payload supports integral with structural elements.
 
WHY: Reduce number of fasteners and/or adhesive required.
 
 
'''Fin Cans'''
 
One prototype printed, downrated to smaller engine size until proven.  Will mount adapter to aft bulkhead using (4) #4-40 screws.
 
= Actual Rocket =
 
The picture above shows a 3D printed 2-part rocket.  65mm max diameter, 29mm motor bay, tangent ogive curve with internal 2-way structural ribs and support for airspeed sensor pitot tube at nose. Made on [[Type_A_Machine|our Type-A Machine]].
 
[[Category:3DPrinting]]

Navigation menu