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|    Message 1,845 of 3,113    |
|    junk@electrosphere.org to Josh Gigantino    |
|    Re: tethers for plane changes?    |
|    29 May 04 04:43:43    |
      Josh Gigantino wrote:       >       > Someplace on the Tethers Unlimited website, Mr Hoyt mentions that the       > MXER tether system cannot be used to make plane changes for tossed       > payloads. Is this a function of that specific design, or a property of       > all proposed tethers? He only mentioned it in passing, could anyone       > explain the orbital mechanics reasons it would not work?       >       > The reason I questioned this is that it seems like a tether designed       > for catapult use could spin up and fire the payload off-axis from it's       > direction of travel. This should provide a change in the payload's       > final orbital plane.       >       > - Josh                            Vertically oriented rotating tethers have extreme difficulty       accommodating payload orbital inclination changes, the exception being a       tether that can reel in and out fully. This is a property similar to       someone trying to rotate a toy gyro in an axis not matching the gyro       rotation axis. It fights you, a lot if the gyro is spinning fast. This       same kind of force is aggravated by the fact that the tether is not a       rigid object.              The reason for the exception is that such a tether could grapple a       payload, reel it and the counterweight in tight, then try to turn to the       payload destination plane, before reeling out again to release. The       problem being, when you reel in, you start spinning really fast       (conservation of angular momentum), which makes it hard to turn the       tether. The reason why this is the exception case is that it is much       easier to turn a compact rotating object than a very wide rotating       object more or less (imagine the tether sweeping out a disk/rotor       shape). The energy to turn the tether is non trivial. The tether would       also suffer from the combination of a drop in center of mass (CM)       altitude and orbital velocity (which is normal for a vertically oriented       tether) and a plane change of it's own when it releases the payload.       This is just a bad problem getting worse.              Try this for a start in an alternative.              http://space.electrosphere.org/explanations              Something like the Southern Cross configuration meets the plane change       need directly, but could be enhanced by use of a CatSling configuration       on the momentum exchange portion of Southern Cross.              --- SoupGate-Win32 v1.05        * Origin: you cannot sedate... all the things you hate (1:229/2)    |
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