Thomas2
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You shouldn't forget that if the central object has a finite mass, the kinetic energy of the weight is not constant anymore but increases/decreases as the wire gets longer/shorter because the central object (e.g. the rocket) loses/gains rotational energy through the pull. It is then dependent on the initial velocity of the weight whether the wire can wind up fully or not. If the initial velocity is not high enough, the kinetic energy of the weight will be used up too quickly and the weight will corotate with the central object before it has fully wound up.krab said:Is that ever cool! It's like my thought experiment of post 25. I was actually trying to solve this case where the central device has a moment of inertia I, and then show how the behaviour changes with I. But the equations are not integrable, so I'd have to do it by a Runge Kutta technique, and the physics gets obscured. My starting condition was that the weights are winding up. But after a while, the central device (let's call it the rocket) will start turning in the same direction, thus stopping the winding up process. I now see that at some point, the rocket reaches a maximum spin speed and then will again slow down as the weights go off to infinity.
Why don't you run your numerical program simply the other way around by simulating the 'rocket de-spin' problem? Just assume that initially the weight is located at the surface of the central object and corotating with it, and then calculate its velocity as the wire gradually unwinds. This gives you then the velocity needed to reversely fully wrap the wire around the object from a given starting radius. One could also determine this analytically from the energy and momentum conservation equations by solving these for the velocity of the weight at a given radius (assuming again that the weight corotates at the surface of the central object).