Why Are Rockets Round? An Exploration

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Discussion Overview

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.

Discussion Character

  • Exploratory
  • Technical explanation
  • Debate/contested

Main Points Raised

  • Some participants propose that cylindrical structures minimize surface area for enclosed volume and provide strength.
  • Others argue that minimizing weight and avoiding sharp corners are important, especially for aerodynamic stability during atmospheric flight.
  • A participant mentions a trapezoidal body shape seen in a design by a major airframer, suggesting it may relate to packaging and aerodynamic considerations.
  • Counterexamples to the notion that all rockets are round are presented, including the Apollo Lunar Module and various thrust vectoring nozzles.
  • Discussion includes the idea that while rockets are often cylindrical, they are not perfectly round, raising questions about the physics behind these design choices.
  • Some participants clarify that thrust vectoring nozzles and rocket nozzles have different design criteria, with few exceptions like the aerospike nozzle.
  • There is mention of cruise missiles that utilize air-breathing reaction motors, which are distinct from rockets in operation and environment.

Areas of Agreement / Disagreement

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.

Contextual Notes

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.

jeffonfire
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Why are rockets round? Why not triangular, would it not be easier to make in some ways?
 
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Cylindrical structures have the least surface area for the enclosed volume, and they are very strong.
 
Minimization of weight as well as pressure vessels do not like sharp corners. Also, rockets do have to fly through our atmosphere before entering space so there is need for aerodynamic stability.
 
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.
 
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.

Probably the implementation of a 'lifting body'.

KM
 
What's a 'rocket' that the Space Scuttle is not, and it is not 'round'? The Apollo Lunar Module was not round.
 
...and the SRBs and the Saturn V that put them into space?
 
I was looking for counterexamples to the universally quantified 'rockets [are] round'.

As the ancillary machinery is conceptually removed, the limit is the nozzle and usually round for reasons cited above. But note the not-round thrust vectoring nozzles on high performance jet engines. Both rocket motors and jet engines are reaction motors.
 
Based on the way physicists usually approach problems, one might wonder why they are cylindrical and not perfectly round, frictionless spheres?
 
  • #10
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.
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.
 
  • #11
They're not both reaction motors?

An "aerospike", indeed, many Trident SLBM have flown.
 
  • #12
minger said:
I've recently seen a design by a major airframer that used a trapdezodial body shape.
Cruise missiles Taurus, AGM-86s ALCM, Storm Shadow; all subsonic powered by air breathing reaction motors.
 
  • #13
Doug Huffman said:
Cruise missiles Taurus, AGM-86s ALCM, Storm Shadow; all subsonic powered by air breathing reaction motors.
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.
 

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