jeffonfire
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Why are rockets round? Why not triangular, would it not be easier to make in some ways?
The discussion explores the design choices behind rocket shapes, particularly focusing on why rockets are typically round rather than triangular or other shapes. It touches on aspects of aerodynamics, structural integrity, and examples of alternative designs.
Participants express multiple competing views regarding rocket shapes, with no consensus on a singular design rationale. The discussion remains unresolved with various perspectives on the topic.
Some claims depend on specific definitions of what constitutes a rocket versus other types of propulsion systems, and there are unresolved questions about the implications of different shapes on performance.
minger said:I've recently seen a design by a major airframer that used a trapdezodial body shape. I can't remember the reasonings, I would assume packaging, but I believe that there were aerodynamic reasons as well. I can't remember the program, but I think it's findable through Google.
The design criteria for a thrust vectoring nozzle and a rocket nozzle are drastically different. The only thing they have in common is the fact that they are attached to a propulsion device. Just about the only rocket nozzle that isn't round is the aerospike and that has never flown.Doug Huffman said:But note the not-round thrust vectoring nozzles on high performance jet engines. Both rocket motors and jet engines are reaction motors.
Cruise missiles Taurus, AGM-86s ALCM, Storm Shadow; all subsonic powered by air breathing reaction motors.minger said:I've recently seen a design by a major airframer that used a trapdezodial body shape.
And have nothing to do with being a rocket. Again, just because they are reaction propulsion, they are completely different in their operation and environment.Doug Huffman said:Cruise missiles Taurus, AGM-86s ALCM, Storm Shadow; all subsonic powered by air breathing reaction motors.