ANGELS DON‘T PLAY THIS HAARP Advances in Tesla Technology
ANGELS DON‘T PLAY THIS HAARP Advances in Tesla Technology ANGELS DON‘T PLAY THIS HAARP Advances in Tesla Technology
implemented on a Motorola 68HC711E9 microcontroller. Due to the intense microwave environment in the vicinity of the rectenna the control system circuitry will be shielded and all exposed wiring will be protected as necessary. Communications The communication subsystem is primarily for downlinking state information from the helicopter to the ground crew. An uplink is desired to provide start/stop and abort signals to the helicopter control system, but may not be feasable. The system will be implimented in infra-red technology. Radio frequency systems are not suitable due to the intense energy enviroment surrounding the helicopter during flight. Conclusion SABER will be a semi-autonomous rotary wing supported platform. All power for SABER will be extracted from an incident 2.45 GHz microwave beam and converted to DC by a rectenna array. SABER will sense all six degrees of freedom from sensors in the incident beam. The control systems will provide stable control and will be robust enough for outdoor demonstration. SABER will promote the concept of microwave power transmission with the general public as a safe and realiable technology. This project is the work of a few dedicated students at the University of Alaska Fairbanks, and the tireless efforts of Prof. Joe Hawkins and Mr. William Brown. References [Contents] [previous] [Feedback] [1] W. C. Brown, Experimental Airborne Microwave Supported Platform, Techniques Branch Rome Air Development Center Research and Technology Division Air Force Systems Command, Griffis Air Force Base, NY, Tech. Rep. RADC-TR-65-188, Dec. 1965. [2] W. C. Brown, Experimental System For Automatically Positioning A Microwave-supported Platform, Raytheon, Burlington, MA, Tech. Rep. PT 1751, June 1968. [3] W. C. Brown, Electronic and Mechanical Improvement of the Receiving Terminal of a Free-Space Microwave Power Transmission System, NASA, Tech. Rep. CR-135194, August 1977. The system to be used by Brown in the wireless transmission of energy to power the craft will be from a 2,45 GHz beam. This will complete a series of tests which he started in 1965. The transmission, and conversion, of this energy is now possible via the APTI patents and HAARP. Raytheon, Brown‘s old employer and the new owner of the APTI patents, was one of three bidders on the HAARP project. Eventually, through a series of corporate buyouts, Raytheon would come to own all of the patents described in this chapter as well as the contract for the second phase of HAARP construction. In the patent it was made clear that this was ―a continuation-in-part‖ of the previous patent by Koert and Cha. This patent describes a system for converting radiofrequency (RF) radiation into DC power using a "cross dipole antenna" which is to be used to receive the RF energy before conversion to DC. This patent carries the power-beaming ideas further, to the point where they can be used.
Previously such systems were impractical because of technical limitations. United States Patent Number 5,293,176 Issued: March 8, 1994 Invented by: Paul G. Elliot. Titled: Folded Cross Grid Dipole Antenna Element. Although it is unknown whether this particular patent was used in the HAARP program, what is known is that the inventor, Paul Elliot, was part of the team identified in the government documents. He obviously brought to the project a high level of knowledge of antenna arrays and related technology. It is not known whether this antenna was intended to be used for sending energy, receiving power or both. This technology is useful in power-beaming systems as well as the other applications described in other patents in this chapter. We speculate that this antenna provided a more efficient system of energy transfer for use in the Eastlund applications. It is possible that, with the antenna gain realized by this design, a larger amount of power could be sent up to the ionosphere. This might be possible from a much smaller antenna field than originally contemplated by Eastlund. United States Patent Number 5,202,689 Issued: April 13, 1993 Invented by: Robert W. Bussard and Thomas H. Wallace. Titled: Lightweight Focusing Reflector For Space. The reflector is intended to complement power-beaming systems previously described in this chapter. According to the patent, ―Large reflectors have many important applications in space. Reflectors can be used, for example, to reflect sunlight onto a solar collector or redirect a microwave power beam‖. The system for the power-beaming described in this patent was designed for sending 10 gigawatts of power. The transmitting, reflecting and receiving system is massive, and the cost of building and using such a system is immense. However, according to the patent, ―The instant invention can be used to transmit power less expensively than the use of microwaves within the Earth‘s atmosphere. It is expected that as the cost of deploying equipment in space decreases, the cost of using the instant invention to transmit power will become lower than the cost of transmitting power using conventional transmission lines. A cost analysis has been performed using cost projections for the 2000 to 2010 time frame. This cost analysis suggests that a principle limiting factor is efficiency and the cost of the radio frequency sources, not the cost of fabricating and launching the reflector‖." The HAARP radiofrequency transmitter, using a focused beam, largely addresses the transmitter-limiting factors described in the patent. The patent goes on to describe the idea of generating energy in locations where it is cheap, and beaming it to areas where energy costs are high. The economic viability is shown, although the size of the project is quite large. The construction of the Trans- Alaska natural gas pipeline has been estimated at over $20 billion dollars, without considering the costs of special ships, off loading facilities and then power generating plants in addition to operating costs. To produce energy at the source and redirect the capital costs of alternate systems to power beaming systems would likely be economically feasible. However, there would be a significant risk to anything flying in the path of the ten-gigawatt beam or if
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Previously such systems were impractical because of technical limitations.<br />
United States Patent Number 5,293,176 Issued: March 8, 1994 Invented by: Paul G.<br />
Elliot. Titled: Folded Cross Grid Dipole Antenna Element.<br />
Although it is unknown whether this particular patent was used <strong>in</strong> the <strong>HAARP</strong><br />
program, what is known is that the <strong>in</strong>ventor, Paul Elliot, was part of the team<br />
identified <strong>in</strong> the government documents. He obviously brought to the project a high<br />
level of knowledge of antenna arrays and related technology. It is not known whether<br />
this antenna was <strong>in</strong>tended to be used for send<strong>in</strong>g energy, receiv<strong>in</strong>g power or both.<br />
This technology is useful <strong>in</strong> power-beam<strong>in</strong>g systems as well as the other applications<br />
described <strong>in</strong> other patents <strong>in</strong> this chapter. We speculate that this antenna provided a<br />
more efficient system of energy transfer for use <strong>in</strong> the Eastlund applications. It is<br />
possible that, with the antenna ga<strong>in</strong> realized by this design, a larger amount of power<br />
could be sent up to the ionosphere. This might be possible from a much smaller<br />
antenna field than orig<strong>in</strong>ally contemplated by Eastlund.<br />
United States Patent Number 5,202,689 Issued: April 13, 1993 Invented by: Robert<br />
W. Bussard and Thomas H. Wallace. Titled: Lightweight Focus<strong>in</strong>g Reflector For<br />
Space.<br />
The reflector is <strong>in</strong>tended to complement power-beam<strong>in</strong>g systems previously<br />
described <strong>in</strong> this chapter. Accord<strong>in</strong>g to the patent, ―Large reflectors have many<br />
important applications <strong>in</strong> space. Reflectors can be used, for example, to reflect<br />
sunlight onto a solar collector or redirect a microwave power beam‖. The system for<br />
the power-beam<strong>in</strong>g described <strong>in</strong> this patent was designed for send<strong>in</strong>g 10 gigawatts of<br />
power.<br />
The transmitt<strong>in</strong>g, reflect<strong>in</strong>g and receiv<strong>in</strong>g system is massive, and the cost of<br />
build<strong>in</strong>g and us<strong>in</strong>g such a system is immense. However, accord<strong>in</strong>g to the patent, ―The<br />
<strong>in</strong>stant <strong>in</strong>vention can be used to transmit power less expensively than the use of<br />
microwaves with<strong>in</strong> the Earth‘s atmosphere. It is expected that as the cost of deploy<strong>in</strong>g<br />
equipment <strong>in</strong> space decreases, the cost of us<strong>in</strong>g the <strong>in</strong>stant <strong>in</strong>vention to transmit<br />
power will become lower than the cost of transmitt<strong>in</strong>g power us<strong>in</strong>g conventional<br />
transmission l<strong>in</strong>es. A cost analysis has been performed us<strong>in</strong>g cost projections for the<br />
2000 to 2010 time frame. This cost analysis suggests that a pr<strong>in</strong>ciple limit<strong>in</strong>g factor is<br />
efficiency and the cost of the radio frequency sources, not the cost of fabricat<strong>in</strong>g and<br />
launch<strong>in</strong>g the reflector‖."<br />
The <strong>HAARP</strong> radiofrequency transmitter, us<strong>in</strong>g a focused beam, largely addresses<br />
the transmitter-limit<strong>in</strong>g factors described <strong>in</strong> the patent.<br />
The patent goes on to describe the idea of generat<strong>in</strong>g energy <strong>in</strong> locations where it<br />
is cheap, and beam<strong>in</strong>g it to areas where energy costs are high. The economic viability<br />
is shown, although the size of the project is quite large. The construction of the Trans-<br />
Alaska natural gas pipel<strong>in</strong>e has been estimated at over $20 billion dollars, without<br />
consider<strong>in</strong>g the costs of special ships, off load<strong>in</strong>g facilities and then power generat<strong>in</strong>g<br />
plants <strong>in</strong> addition to operat<strong>in</strong>g costs.<br />
To produce energy at the source and redirect the capital costs of alternate systems<br />
to power beam<strong>in</strong>g systems would likely be economically feasible. However, there<br />
would be a significant risk to anyth<strong>in</strong>g fly<strong>in</strong>g <strong>in</strong> the path of the ten-gigawatt beam or if