FactChecker
Science Advisor
Homework Helper
- 9,327
- 4,618
hutchphd said:Here's one. https://second.wiki/wiki/falacia_del_cohete_pc3a9ndulo
And a video
The crux here is that the thrust vector for a rocket is rigidly attached to the rocket. If you could always pull the nose up then you would stabilize but that is not easy to do. Goddard figured this out pretty quickly as I recall. (I read his biography 60 years ago! )
A first thought:
If the thrust is stabilized to always point in the desired direction of travel, the "puller" position would have some stability. A "pusher" position would require the vectoring to point even farther from the desired direction than the rocket is pointing.
Of course, if the steering is done with fins, then vectored thrust is not an issue. It might not take much velocity for the aerodynamic forces to be more powerful than thrust vectoring.
Last edited: