On the feasibility of orbiting satellites
As with my first post on rocketry in a vacuum (
http://cluesforum.info/viewtopic.php?p=2404517#p2404517) I am aiming to get at the essence of why the orthodox narrative cannot be the reality in question. A perfect example of such, which I'm sure all of you are familiar with, is that a hollow aluminum body cannot slice through steel and concrete, and so we can say without a shadow of a doubt, that the 2001 psyop event was fraud, no "occam's razor" needed.
I wish to crystalize the magician's deceit and expose the illusion once and for all. There has been a great wealth of discussion on this thread, and any thinking being who has read through it would surely have developed hearty suspicion if not downright incredulity against the official claims of satellites. However, I think that there is a critical point which has gone unsaid or has been understated which needs to be addressed.
In order for a satellite to theoretically sustain orbit it must attain speeds upwards of 27,000 kilometers per hour. If anyone plans on doing calculations regarding the point I will make, let us say that the satellite is traveling 30,000 kilometers per hour. The rounded numbers will make for ease of mathematical analysis.
Now anyone who is familiar with Newton's law of gravitation knows that the force of gravity exerts itself on every part of an object independently and that the sum of these forces are understood as acting as a whole on the object's
center of gravity. Were satellites designed as a cohesive sphere or some other polyhedral shape, then the point I am about to make would be poor. But, most of these designs are highly elongated shapes which could never withstand the inertial forces that they would be subjected to. Consider some examples:
The International Space Station
Orbiting Carbon Observatory 2
Jason 1
Sentinel 3
In these designs we see particular tension points where two large components of the object are held together by something like a small rod. These rods would supposedly function to balance any differential of forces that would be exerted on the respective components they hold together. But, there is no material on Earth which is strong enough to withstand the forces required by such designs. Specifically, I am referring to the centripetal force, which is related to the “push” one experiences when one goes around a sharp turn in a car.
It seems many people are under the impression that once a certain velocity is attained by a satellite it will be smoothly set into orbit never to be disturbed by the forces of gravity again. They must not know that an orbiting object would have an elliptical orbit, not a perfectly circular one and that even discounting the motion of the Earth, such an elliptical orbit would regularly accelerate and decelerate such an object. However, the Earth itself is not stationary, and in fact it has a tangential velocity of about 100,000 kilometers per hour as it moves around the Sun and it also has an elliptical orbit where when it is closer to the Sun it moves faster and when it is further from the Sun it moves slower.
Consider the scenario where an orbiting satellite with an average velocity of 30,000 kilometers per hour is moving along the opposite vector as the tangential vector of the Earth as it is traveling around the Sun, a situation which would occur once per orbit. At this instant the orbiting object and the Earth are moving away from each other at around 130,000 kilometers per hour, and as momentum must be conserved, this would cause a rapid deceleration of the orbiting object and this rapid deceleration would not be experienced evenly through the entire object, since it’s respective components would have different mass and with different mass there would different magnitudes of the centripetal force acting upon them. It is then the job of the small rods to handle the stress of transferring these forces through the components it holds together. But, the centripetal force is governed by the equation:
and the velocity at that instant would be 130,000 kilometers per hour, which means even a tenth of a percent difference in the mass of the two components would result in the more massive component being subjected to a force much greater than the less massive component. So, if even the lighter component had a mass of 1 kilogram and the heavier component had a mass of 1.001 kilograms then the rod would be subject to a 1,000,000 Newtons at this instant which is about 225,000 pounds of force. But, no material on Earth could allow for a single rod to uphold 225,000 lbs without failing, and the claimed satellites would have components which would have mass differentials much greater than a hundredth of a kilogram, and so the official narrative would require these rods to be subjected to forces many times greater than 225,000 pounds of force.
Therefore, even if it were practically possible to attain the extravagant speed and altitude necessary for orbit, such an object as those above would be instantaneously ripped apart.
Let us be clear then that were any of the above objects to orbit at all, they would orbit in pieces.
In my personal opinion, some of these designs look so flimsy I wouldn't trust walking under them on a windy day.