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I have obliged their request, except to quote the above paragraph. My suggestion to them was the following:
As for whether you work for NASA or not, the website has a nasa.gov address. So if you’re not affiliated with NASA then I suggest you find a different website address, since otherwise, you are misleading the public. Of course, we can avoid all this extracurricular activity if you, as an astrophysicist, would tell us why a geocentric system would not work. The ball is in your court.
To this day there has been no response from them. As one can see quite readily from the above exchanges, although one government agency, at least in a private letter, was willing to divulge the truth about the use of fixed-Earth mechanics, another agency refused to be as forthcoming when the audience included the millions of potential readers on the Internet. This is really no surprise to us. Those who control our space programs have a vested interest in keeping the public under the illusion of Copernicanism, since all their funding and projects are based on Copernicus’ premises, including the quest to find life in other worlds. Only those who are courageous and knowledgeable enough can expose the illusion and allow the public to see the cosmic shell game that has been occurring for quite a long time. One such party is the team of Ruyong Wang and Ronald Hatch, two former government satellite engineers who know the truth about the illusion. In one of their investigations on the Global Positioning System they write:
…NavCom Technology, Inc. has licensed software developed by the Jet Propulsion Lab (JPL) which, because of historical reasons, does the entire computation in the ECI frame. Because of some discrepancies between our standard earth-centered earth-fixed solution results and the JPL results, we investigated the (name removed by moderator)ut parameters to the solution very carefully. The measured and theoretical ranges computed in the two different frames agreed precisely, indicating that the Sagnac correction had been applied in each frame.
As the discussion of the Sagnac effect indicates the fundamental question regarding the speed of light is the following: Is the speed of light constant with respect to the observer (receiver) or is it constant with respect to the chosen inertial ECI frame? Clearly the GPS range equation indicates the speed of light is constant with respect to the chosen frame…The JPL equations, used to track signals from interplanetary space probes, verify that the speed of light is with respect to the chosen frame. In the JPL equations, the chosen frame is the solar system barycentric frame….Clearly, the JPL equations treat the speed of light as constant with respect to the frame – not as constant with respect to the receivers.[3]
In other words, the Jet Propulsion Laboratory (JPL) employs the Earth Centered Inertial frame (ECI) for probes sent out near the Earth (as does NASA and the GPS), yet the Jet Propulsion Lab claims to use the “solar system barycentric frame” for deep space navigation. Wang and Hatch tell us, however, “the Jet Propulsion Lab…because of historical reasons, does the entire computation in the ECI frame.” Not only does the Jet Propulsion Lab use the ECI frame exclusively, Wang and Hatch tell us that the Lab corrects the calculations in its “solar system barycentric frame” so that they match the ECI frame! We can see clearly that the Earth-centered frame is the standard, and thus, use of the ‘solar system barycentric frame’ is superfluous. Once the Lab’s computer makes the corrections to the solar system barycentric frame, in reality the deep space navigation is actually using the ECI frame – a fixed Earth. The public wouldn’t have been made privy to this sleight-of-hand manipulation except for the fact that two knowledgeable insiders, Wang and Hatch, have told the real story. In effect, the Earth Centered Inertial frame (e.g., geocentrism) is the only frame that allows the GPS and various space probes to work properly. The significance of these facts will be highlighted when we deal with the Sagnac Effect in Chapter 5, and the Global Positioning Satellites in Appendix 6.
As for whether you work for NASA or not, the website has a nasa.gov address. So if you’re not affiliated with NASA then I suggest you find a different website address, since otherwise, you are misleading the public. Of course, we can avoid all this extracurricular activity if you, as an astrophysicist, would tell us why a geocentric system would not work. The ball is in your court.
To this day there has been no response from them. As one can see quite readily from the above exchanges, although one government agency, at least in a private letter, was willing to divulge the truth about the use of fixed-Earth mechanics, another agency refused to be as forthcoming when the audience included the millions of potential readers on the Internet. This is really no surprise to us. Those who control our space programs have a vested interest in keeping the public under the illusion of Copernicanism, since all their funding and projects are based on Copernicus’ premises, including the quest to find life in other worlds. Only those who are courageous and knowledgeable enough can expose the illusion and allow the public to see the cosmic shell game that has been occurring for quite a long time. One such party is the team of Ruyong Wang and Ronald Hatch, two former government satellite engineers who know the truth about the illusion. In one of their investigations on the Global Positioning System they write:
…NavCom Technology, Inc. has licensed software developed by the Jet Propulsion Lab (JPL) which, because of historical reasons, does the entire computation in the ECI frame. Because of some discrepancies between our standard earth-centered earth-fixed solution results and the JPL results, we investigated the (name removed by moderator)ut parameters to the solution very carefully. The measured and theoretical ranges computed in the two different frames agreed precisely, indicating that the Sagnac correction had been applied in each frame.
As the discussion of the Sagnac effect indicates the fundamental question regarding the speed of light is the following: Is the speed of light constant with respect to the observer (receiver) or is it constant with respect to the chosen inertial ECI frame? Clearly the GPS range equation indicates the speed of light is constant with respect to the chosen frame…The JPL equations, used to track signals from interplanetary space probes, verify that the speed of light is with respect to the chosen frame. In the JPL equations, the chosen frame is the solar system barycentric frame….Clearly, the JPL equations treat the speed of light as constant with respect to the frame – not as constant with respect to the receivers.[3]
In other words, the Jet Propulsion Laboratory (JPL) employs the Earth Centered Inertial frame (ECI) for probes sent out near the Earth (as does NASA and the GPS), yet the Jet Propulsion Lab claims to use the “solar system barycentric frame” for deep space navigation. Wang and Hatch tell us, however, “the Jet Propulsion Lab…because of historical reasons, does the entire computation in the ECI frame.” Not only does the Jet Propulsion Lab use the ECI frame exclusively, Wang and Hatch tell us that the Lab corrects the calculations in its “solar system barycentric frame” so that they match the ECI frame! We can see clearly that the Earth-centered frame is the standard, and thus, use of the ‘solar system barycentric frame’ is superfluous. Once the Lab’s computer makes the corrections to the solar system barycentric frame, in reality the deep space navigation is actually using the ECI frame – a fixed Earth. The public wouldn’t have been made privy to this sleight-of-hand manipulation except for the fact that two knowledgeable insiders, Wang and Hatch, have told the real story. In effect, the Earth Centered Inertial frame (e.g., geocentrism) is the only frame that allows the GPS and various space probes to work properly. The significance of these facts will be highlighted when we deal with the Sagnac Effect in Chapter 5, and the Global Positioning Satellites in Appendix 6.