（IV-ii）Common Engine and Flying Saucer Engine
Special noun and item: Flying saucer engine, PNT activation mechanism, Milk hitchhike-able speed，non-milk hitchhike-able speed, self-propelled engine, almsgiving-style engine, PNT activation source material, low-intensity train flying saucer engine, flying saucer engine generator( volitional PNT generator), PNT activated current.
[Preface]: My general intention to write this section is to refurbish the conventional rational sense on “engine” and “kinetic energy” of people, and trying to activate and exploit the active exploration eyeshot of people.
Although, we had practical masterdom and utilization of nuclear energy in prior, while the very thing did not ever place a premium on and stimulate further logos regeneration sensitively; on the contrary, it was rashly ranked into relativity by the so called authority without any more concern.. The conventional experience and authoritative logos still estoped some of our significant exploration eyeshot, and desolated some new logos germination which should be germinated earlier by its sanctification. And indeed, the gist Homogenous Cosmos Originated from Unique Gene resorts to refurbish the conventional logos of people is entirely derived from the rational re-cognition and redefinition of “cosmic matter”, “space-time”, “motion” and “kinetic energy”.
(1) About common engine
Once we refer to “engine”, we can sensitively associate with internal-combustion engine, turbo，electrical motor etc. According to our general experience and conventional sense, we can haply obtain a simple definition of engine like this: so-called “engine” is but a kind of mechanism with function to transmute and transfer some of the advantageous kinetic energy or potential energy of energy source material to load objects constantly as kinetic energy. On the view of the energy origin, the general energy resources are generally fuel chemical energy, geopotential energy, electric energy, nuclear energy etc. On the view of the dynamic mechanism for common engine to drive, we are generally convenient to adopt the very energy resource material with remarkable advantageous kinetic energy to collide or extrude the proper load objects so that some of the advantageous kinetic energy of the energy resource material can be transferred to the proper load objects consequently. For instance, steam engine depends on running vapor collision to work; internal-combustion engine depends on the burning gas extruding the plunger working; wind-power or water-power generator depends on the running airflow or stream collision working; rocket depends on the jetting gas recoil working, … ….
In a summary word, the most typical dynamic characteristics of common engine is that it depends on mutual collision or extrusion to transfer advantageous kinetic energy from energy resource material to the load objects. In another word, we are generally used to procuring engine by adopting one object with advantageous kinetic energy or potential energy to collide or extrude or recoil the proper load object. As a result, the working dynamic process of common engine can be accordingly expressed mathematically as following:
For the convenience to describe the process mathematically, we just denote the very mass of the energy source material as m1, the mass of the proper matter field as M1; just denote the mass change of m1 as Dm1 and denote the mass change of M1 as DM1 during the course of the energy source material releasing energy; and at the same time, the energy source material works to the load object synchronously, consequentially, there must be a certain quantity of cosmic mass transmuting and transferring from energy source material to the proper load object, we just denote the proper quantity of the mass transition as ΔM’1（ΔM’1﹥0） Then the unbalanced inertial conservation equations of the energy source material can be consequently formulated as following:
Then the acceleration of the energy source material can be formulated as following:
The velocity of the energy source material can be formulated as following:
For certain convenience, we just denote the mass of the load object as m2, the mass of the matter field of the load object as M2; and denote the mass change of m2 as ΔM2 and the mass change of matter field M2 as ΔM2 during the course of the load object driven by the energy source material. As the change of M2 directly derives from the input ΔM’1 of the energy source material, under the precondition that the load object does not bear any outside resistance, ΔM2 and ΔM’1 satisfies ΔM2=ΔM’1. For the convenience, we just directly take ΔM’1 instead of ΔM2, and then the unbalanced inertial conservation equations of the load object can be consequently formulated as following:
Then the acceleration of the load object can be formulated as following:
Then the velocity of the load object can be formulated as following:
If the above drive systems are internal-combustion engine, jet plane, or rocket etc, the energy source material here is burning fuel or high temperature jetting gas, the load objects are the plunger, turbine and all the driven material system connected to the plunger or turbine ----- car, or plane, or rocket etc. If the drive system is electrical motor, then we can treat the conductors or the conductive atoms or radicel as the energy source material, and the load objects are just the motor rotor and all the material mechanism connected to the rotor. If the drive system is common nuclear energy system, then the energy source material are the fissioned or aggregated nucleus, and the load objects are of course the material objects impinged by the nuclear radiation.
Engines like these, one hand, as the kinetic energy of the energy source material is usually rather limited, and what’s more, the energy transference effect is proportionally weakened so much by the manner of mutual collision or extrusion for energy transference from energy source material to load object during the course of the moving speed of load object coming to close the moving speed of the energy source material. ------ For instance, the closer the flying speed of the rocket and the flying speed of the jetting gas is, the rocket is more difficult to accelerate continuously. As a result, if we do not essentially innovate on the engine working dynamic mechanism, no matter how much we try to and enhance functions optimize the framework of rocket, or enhance the jetting speed, the flying speed of rocket can not be improved remarkably.
Just the same of cosmic matter, and just exist in similar space-time, why the jetting gas molecules from rocket, the electrons around the atomic nucleus even the photons in space can go that fast, comparably, while the man-made rocket flying speed is that low!? Is it just because of the special favor of nature?
Of course, the rootstock is not the special favor of nature. Considered by Homogenous Cosmos Originated from Unique Gene, all cosmic matter in space-time are innately generated according to law of identity of nature, and consequentially, the dynamic characteristics of any matter in cosmos are equivalent, just as the potential energy of a kilogram of uranium and a kilogram of earth are critically equivalent. With a kilogram of uranium and a kilogram of earth, in order to procure the same energy exploitation effect, the key problem is only how we try to exploit them according to their individual physical characteristics. On “engine”, the key issue only exists in our traditionary drive method ----- the foundational driving dynamic mechanism. In fact, as cosmic matter; the connatural essence of the rocket and the fuel which rocket depends on recoiling as energy source material are just the same, and their existence and motion status in space-time are essentially determined by the PNT of their matter system in identity. Just because history ignorance, we did not pay our special attention to it, we did not intentionally try to activate the potential energy of the rocket itself as cosmic matter, but to depend on the recoil derived from the jetting gas, because in fact, as the special physical characteristics of fuel molecule, some of its potential energy is very easy for us to exploit and use (Ignition is OK then), as a result, it is very easy and convenient for us to adopt it as energy resources. We have to admit it’s a “favor” we get from the nature.
Our teeth have not grown up, while we luckily meet the tender bean curd arranged around us by the nature in prior, it’s of course good luck of human!
Considered from obvious fact, the rotation and revolution of the earth do not originally depend on any format collision or extrusion, the free motion of any single molecule does not originally depend on any collision … …； high speed running electrons around atomic nucleus do not originally depend on any collision, transmission of photon does not originally depend on any collision too. It’s obviously easy for us to draw our conclusion that there is none essential logic relationship between “collision” and “motion or acceleration”; and collision is of course not the patent of drive, although collision is feasible for objects with different kinetic energy to transfer kinetic energy mutually and it is very feasible to produce mutual recoil indeed. Consequently, it is obviously not the root cause for matter system to accelerate. Considered by Homogenous Cosmos Originated from Unique Gene, motion status of matter system essentially depends on the conditions of PNT of matter system, it is just the reality of nature.
Then considered from the view of the variation of of matter system, what is the microcosmic physical mechanism of nuclear fission and the fuel burning?
Can we directly inoculate the microcosmic physical mechanism onto the rocket body, so that the rocket needs none special supplemental fuel and works like self-burning recoil, and is able to fly as fast as high speed jetting gas molecule even as fast as the electrons around atomic nuclear or the photon in vacuum? … …。
Can we produce flying saucer engine with uranium or similar matter as uranium, but not A-bomb only?
This is what I’d like to introduce about “flying saucer engine” next.
（2）Dynamic principia of flying saucer engine
It has been introduced in prior, any cosmic matter, as long as they exist in space-time, they must have the absolute space-time momentum P=mV=d(M←m)*Y, and in cosmos, no matter normal motion or wave-form motion of matter system, motion status essentially depends on the condition of PNTof matter system.
Since the motion status essentially depends on the PNT condition of matter system, then can we manage to govern and control the PNT condition of matter system volitionally, so that we can predominate the motion status of any matter system expediently?.
Flying saucer engine is just deduced from the natural principia. In a simple word, so-call “flying saucer engine” is just a dynamic activation mechanism; which can be used to activate and control the PNT condition of matter system directly, so that it can be used to govern motion status and exploit potential energy of cosmic matter according to connatural behavioral characteristics of nature itself. Of course, here the “control of PNT condition” generally means to govern the magnitude of the both coexisting and reverse taches d(M→m) and d(M←m) of matter system by certain feasible way。
Generally, in order to activate the potential energy of matter system so that the matter system can move faster and faster, we have to manage to increase the magnitude of d(M←m) of matter system, so as to keep d(M←m) bigger than d(M→m), matter system accelerates accordingly. And on the other hand, in order to decrease motion speed of matter system expediently, we usually have to manage to decrease the magnitude of d(M←m) or keep the magnitude of d(M←m) smaller than d(M→m) besides removing or releasing some of its kinetic energy outside, so as to passivate and calm the potential energy of matter system efficiently.
Now let’s suppose there is a matter system (we can also suppose it is just our flying saucer engine), its positive mass is m, and the proper matter field mass is M, in order to govern the motion status of the matter system, we just manage to adjust and control the magnitude of the both coexisting reverse transmutation taches d(M→m) and d(M←m) of matter system. As the implementation of the adjustment of the magnitude of d(M→m) and d(M←m), both the positive mass m and negative mass M of matter system will vary accordingly. We just denote the variation of m with time t into function format as m(t), and denote the variation of M with time t into function format as M(t). Then the unbalanced inertial conservation equations of the matter system can be consequently expressed as following;
Then, during the course of the matter system PNT being adjusting, the acceleration of matter system can be accordingly formulated as following:
During the course of the matter system PNT being adjusting, the velocity of matter system can be accordingly formulated as following:
For further concretion, we suppose there is a flying saucer engine starting from the surface of the earth, and ultimately, it adjusted its negative and positive mass quotient K off its initial value 0.001, and here, let suppose the Time Dynamic Speed Y(t) of matter system is just a constant of the same as light speed 3.0X108M/S (In fact, time dynamic speed is bigger than light speed), then, we substitute the proper values into the velocity equation, we can consequently obtain the flying speed of the flying saucer engine as following:
(Among the equation above, V0 represents the initial speed when the flying saucer stopped on the surface of the earth; K0 represents the initial negative and positive mass quotient of matter system when the flying saucer engine stopped on the surface of the earth.)
It implies when the flying saucer engine adjusted its negative and positive mass quotient K off its initial value 0.001, its flying speed has approached 3.0X105M/S relative to the earth. Accordingly, if the flying saucer engine goes around a circle of the earth on the synchronous satellite orbit at the very speed, it will only cast it X.XX hours; taking this flying saucer engine and just flying at this speed, it will only cast us about 11 days to travel a circle from the earth to the sun. Obviously, the flying speed is rather remarkable compared to the flying speed of common aircraft, missile, satellite etc. what’s more, as the remarkable maneuverability advantage of flying saucer engine, if we just adopt such a flying saucer engine to hunt common plane or missile, even military satellite, it may be even easier than glede hunting chicks.
Of course, as the variation of the negative & positive mass quotient K, many relevant physical phenomena will occur consequently.
As the further variation of the negative & positive mass quotient K, many volitional control parameters of flying saucer engine will consequentially become more and more critical and difficult, because with the variation of the negative & positive mass quotient K, the existing state of matter system will vary accordingly. Theoretically, if the flying speed of flying saucer engine can approach the speed that electrons usually do, then the material existing state of the flying saucer engine must have been very similar to electrons; it indicates the flying saucer engine has been adjusted into a sheaf of electrons; if the flying speed of flying saucer engine approaches the speed of light, then the material existing state of flying saucer engine must have been the same as photon, that’s to say, the flying saucer engine must have been volitionally adjusted into a sheaf of light. At the same time, during the course of the volitional adjustment and control of PNT, the compositive material (atom/nucleon) of flying saucer engine will wear off some of its positive mass for activation radiation, or appear seriously thermal distortion, even it may be bombed like TNT bomb or A-bomb if the activation escaped from our volitional control unexpectedly. .
In practical hitchhiking, relative to the variation of the negative & positive mass quotient K, vitality mechanism of organism is sensitive and frangible, because any object with positive mass, as long as it is hitched on the flying saucer engine, the negative & positive mass quotient K of the hitched object must keep consistent with the flying saucer engine. To any organism, as the variation of the negative & positive mass quotient K, the state equations and mechanics structure of any atom made of the organism which hitched on the flying saucer engine will consequently vary accordingly; it implies the physical and chemical characteristics of the compositive atoms will vary sensitively, of course, it will impact the biological property and function of the organism. Even for some certain necessity, we must fix some certain electronic device on flying saucer engine; we still have to consider the influence deriving from variation of the negative & positive mass quotient K of flying saucer engine.
For some certain convenience, we just treat a cup of milk as a type of organism; and define the speed range of flying saucer engine which does not intensively impact the biological property and function of organism as “milk hitchhike-able speed”. For instance, if we want to spend weekend on the moon or travel to any other planet in solar system, we then have to consider the milk hitchhike-able speed for the trip; if we’d like to involve exploration out of solar system, I’m afraid, we then have to consider the non-milk hitchhike-able speed.
Now, as the verification of the flying saucer engine dynamic principia, let’s obtain a primary definition of flying saucer engine.
In a summary word, so-called “flying saucer engine” is but a mechanism and way which human use to immit volition control into PNT process of matter system ----as the existence and motion status of any matter in space-time is essentially and proportionally determined by the corresponding PNT conditions of matter system, by immitting volition into PNT process of matter system, we can expediently govern and predominate the kinetic status of matter system by the connatural behavioral way.
In a detailed word, it is to inoculate certain PNT activation mechanism onto the proper flying saucer engine activation source material, by the governance of the PNT activation mechanism to predominate the PNT status of the matter system of the flying saucer engine activation source material, so that we can control the kinetic status of the flying saucer engine activation source material volitionally. On the view of the engine drive mechanism and energy source, flying saucer engine is typical self-propelled engine, while common engine is just the almsgiving -style engine comparably.
(3) Several difficult technological problems of flying saucer engine
Considered by Homogenous Cosmos Originated from Unique Gene, all matter in cosmos can never break away from space-time and renegade from PNT relationship. While the sustainment and prosecution of PNT of matter system is connatural behavior of nature, connatural behavior of nature is not always enough to satisfy the volitional requirements of human, in many cases, for some certain necessity, we have to consider the volitional adjustment and control of PNT of matter system.
Meanwhile, are there positive possibilities for us to volitionally intervene and adjust PNT process of matter system?
If there are some possibilities, then how can we practically intervene and control the PNT process of matter system?
What kind of mechanics configuration of source material is convenient for us to interne and control PNT process of matter system?
What kind of control way or method is more expedient and efficient for us to do it?
① The discovery and foundation of PNT activation mechanism of matter system
Moving speeds of comprehensive matter in the nature are
usually different, and all moving speeds of matter in cosmos can be changed; and
substantively, the change of moving speed essentially depends on the proportional
variation of PNT of matter system. It of course implies that the PNT process of any matter
system is variable, and indeed, there is connatural behavioral mechanism to make PNT vary
accordingly. The key issue is that we still do not know what the connatural behavioral
mechanism is and how we can practically master the behavioral mechanism, although there
are so many objects accelerating around us.
Then, under the certain space-time, what a transmutation and transference process of certain genes the PNT of matter system contains?
On the view of PNT process variation or implementation
mechanism, what a connatural PNT implementation mechanism and variation process the fuel
gets burning? How the nucleons get fission and release energy? What illuminations can the
proper PNT variation process shows us?
What kind of material mechanics conformation is convenient for us to intervene and control the PNT process of matter system?
Undoubtedly, further study and verification of these issues will consequently do a lot good to the discovery and instauration of the PNT volitional activation mechanism.
② Entirely volitional control of PNT of matter system
Under normal space-time condition, cosmic matter generally exists in space-time in mechanics frame of atom. And indeed, we are usually convenient to make use of the material consisting of elementary atoms but not the “neutron mass”, “proton mass” or “electron mass”. Obviously, the discovery and consummation of “state equations of atom in space-time” will bring us remarkable convenience for our practice. In order to illuminate the proper problems concretely, here, we just try to illuminate the technological problems of flying saucer engine by the instance that we adopt the flying saucer engine activation source material consisting of certain atom mechanics system.
It implies that we just treat mechanics configuration of certain atom system as our mechanics object to study the PNT activation. Considering the connatural pertinent mechanics logic relationships of internal atomic nucleus, atomic nucleus and electrons around atomic nucleus and any contiguous atoms in atom system, and the connatural properties determined by these pertinent mechanics relationship, during the course of the practical PNT activation control, we must consider the both hierarchies of the mechanics effect, ——pertinent mechanics effect within atom and pertinent mechanics effect between continuous atoms, including the PNT activation mechanics effect of internal atom, PNT activation mechanics effect of electrons around nucleus, PNT activation pertinent mechanics effect between atomic nucleus and electrons around the atomic nucleus and PNT activation pertinent mechanics effect between any two continuous atoms in atom system.
For the convenience to illuminate the problem in a simple way, we suppose that the flying saucer engine source material is just an atom system consisting of an atom A and an atom B, and we denote it as “A-B”. (Of course, the both atom A and atom B may be the same element, and may be different elements too) We just illustrate them as following:
(The small dark brown circle in the centre represents the atomic nucleus, the light blue circle around represents the electron cloud)
As the connatural mechanics configuration of atom, ——the performance of PNT of nucleus and electrons in atom is almost relatively separated. Let’s suppose that there are N1 nucleus and N2 electrons in an atom, and at the same time, we denote the mass of each nuclear as m1 and the mass of the proper matter field as M1, and denote the mass of each electron as m2 and the mass of the proper matter field as M2, then, we can arrive at:
First, observed inside the atom, the constitutes of absolute space-time momentum of atom is ①+②+③
① Absolute space-time momentum of separate nuclear is: N1*（m1*V1）=
② Absolute space-time momentum of separate electron is: N2*（m2*V2）= N2*d(m2→M2)*Y(t)
③ Absolute space-time momentum of the whole atomic nucleus is: (N1m1)*V3= d(N1m1→N1M1)*Y(t)
(Among the equations above, V1 represents the moving speed of separate nuclear, V2 represents the moving speed of separate electron, and V3 represents the moving speed of the whole atomic nucleus)
Second, observed out of the atom, besides the three items above, the absolute space-time momentum of the atom still includes the item ④:
④ The integrity absolute space-time momentum of atom:
Third, if the flying saucer activation source material is an atom series of “A-B”, then equation
will be changed into:
Among the equations above, V4 represents the moving speed of atom or atom system; it is just the objective speed we are trying to procure and predominate, V1 V2 V3 are just the speeds we have to consider to regularize and restrict for the feasibility and safety of the atomic nucleus PNT activation. The bigger the speed of V4 we can procure, and the more optionally we can control the adjustment of V4, the better the flying saucer engine is.
Then, how can we enlarge and control the magnitude of V4 efficiently?
Of course, we can consider the PNT activation of both the electrons around atomic nucleus and the atomic nucleus. Meanwhile the moving speed of the electrons around atomic nucleus is rather bigger, and almost all electrons move along inconstant curve orbits, only tracking them is very difficult, no more critically orientated PNT activation, and the mass of electron is rather tiny; it of course indicates poor potential energy for activation, what’s more, the PNT activation of electrons around the atomic nucleus directly impacts the stabilization of the macroscopical mechanics configuration of atom system, it is very sensitive to cause excessive thermal expansion, radiation, unfreezing, evaporation and even burst into pieces, it will vitally impact the stability and safety of the flying saucer engine, these indicate that electrons around atomic nucleus are not ideal for PNT activation, as a result, we have to turn to consider the PNT activation of atom nucleus.
Compared to the electrons around the atom nucleus, the atomic nucleus is rather massive; it of course implies rich potential energy for PNT activation, and linked by strong force, the atomic nucleus is rather solid, it of course indicates the perfect anti-jamming capability for PNT activation, and what’s more, atomic nucleus has connatural advantage to govern the electrons around it, when the atomic nucleus are activated for volition PNT adjustment, it’s very convenient and easy to hold down the electrons around it to move synchronously and proportionally but not to disturb the normal distribution of the electron cloud intensively, this is of course very good to the stability and safety of the flying saucer engine. All in all, it seems that atomic nucleus is much more advantageous than electron cloud for PNT activation. As long as we can expediently activate the atom nucleus, and the atom nucleus can hold down the electron cloud in regular way synchronously, and we can ensure the consistency of the PNT activation orientation and the PNT activation strength of proper atom system, we then succeed consequently.
Of course, the advantages of the atomic nucleus are relative to the electron cloud around it, when the atomic nucleus is activated for volitional PNT adjustment, because of the inevitable mechanics variation or deviation of the atom nucleus, and because of the connatural pertinent mechanics effect in atom system, it maybe cause series harmful effects accordingly, for instance, as overload PNT activation or irregular PNT activation, the atom nucleus occur destructive mutation or fission, or the electron cloud was disturbed too much for some certain pertinent mutation of atomic nucleus so that the macroscopical material status deviated too much. And of course, these harmful effects will consequentially impact the feasibility and the safety of the flying saucer engine, and maybe even vitally restrict the range of the adjustable value of V4, as a result, we have to consider the following two relevant technologies.
First, control of critical consistency of PNT activation orientation and critical equilibrium distribution of PNT activation strength during the course of flying saucer engine being activated
First, during the course of the flying saucer engine being activated, critical consistency of PNT activation orientation is rather beneficial and efficient for oriented driving; second, critical consistency of PNT activation orientation and critical equilibrium distribution of PNT activation strength can prevent flying saucer engine being torn or burst into pieces for rough activation, because, if the flying saucer engine activation source material is built of atomic mechanics conformation, obviously, when the PNT of matter system of activation source material is activated, the equilibrium distribution of PNT activation strength discrepancy between any two continuous atoms or any two neighbor radicel mechanics units can never exceed the restriction of the original polymerization force between any two continuous atoms or neighbor radicel mechanics units, otherwise, the flying saucer engine will be torn into pieces or bombed like an A-bomb.
During the course of the activation of PNT of matter system, the higher quality the control of critical consistency of PNT activation orientation and critical equilibrium distribution of PNT activation strength is, the better orientated driving effect of the flying saucer engine consequently is and the bigger the safe coefficient of flying saucer engine is. As a result, under the precondition that we have primarily mastered the volitional activation mechanism of PNT of matter system, the efficient control of critical consistency of PNT activation orientation and critical equilibrium distribution of PNT activation strength is of course the next major subject we should engage in.
Second, the restriction control of the activation radiation ullage, thermal distortion, thermal dispelling of flying saucer engine
Generally, when the flying saucer engine is activated, as the activation variation of the connatural mechanics configuration in atom system and the connatural pertinent mechanics logic in the atom system, some of the characteristics of atomic nucleus or atom system will inevitably change, the component atoms of the flying saucer engine may radiate accordingly, it will of course wear off some of the mass or energy of the flying saucer engine, even may seriously influence some of the physical characteristics or functions, impact the stability and reliability of the flying saucer engine function, and at the same time, in military occasion, it is very easy to be found and incur attack strategically.
It implies that the restriction of the radiation ullage of the flying saucer engine derived from PNT activation is still a very important technological factor. The higher quality the radiation ullage restriction is, the better the drive effect and efficiency is, and the more steady and reliable the flying saucer engine function is, the flying saucer can consequently last longer.
Of course, besides the two technological factors above, it is still very necessary for us to consider the maneuverability control of flying saucer engine.
The maneuverability control of flying saucer engine usually means the control sensitivity and accuracy of the magnitude of d(M→m) and d(M←m) of matter system. Generally, in order to ensure the control sensitivity and accuracy of flying saucer engine, we are convenient to choose the matter block with homogenous and steady physical characteristics as the PNT activation source material.
Of course, we can enhance the maneuverability by multiple possible ways, for example, we can design the geometrical profile of flying saucer engine like a saucer, thus, one hand, it is convenient for the flying saucer engine to accelerate at random orientation without special swerve during the course of the driving; on the other hand, the saucer geometrical profile can ensure the flying saucer engine with certain mass occupies least space volume when it rotates. And at the same time, once it is necessary to decelerate, it can keep itself in a more active energy state by rotating itself, and just to keep the negative and positive mass quotient K of the flying saucer engine in a bigger value, so that once it is necessary for the flying saucer engine to accelerate, it can expediently translate the rotation repertory energy into linear motion kinetic energy, thus, it has not only actualized the intention of maneuverability drive control, but also obviated the suspicion of trying to accelerate in a sudden but ability not equal to its ambition, and it obviates the risk of being bombed for rush activation.
In summary, the realization of flying saucer engine technology demands us to consider the foundation of the PNT activation mechanism and make choice of the ideal PNT activation source material first, and if necessary, we have to consider the mechanics structure optimization readjustment or reorganization for the benign activation and maneuverability of the activation source material, then inoculate the proper PNT microcosmic activation mechanism onto the activation source material. Obviously, no matter the foundation of the activation mechanism or the choice of the ideal activation source material, or the necessary mechanics conformation optimization readjustment or reorganization, or the design and inoculation of the PNT microcosmic activation mechanism, the dependence to the naissance of atom state equations in space-time is of course self-evident
The thought framework of PNT activation control technology can be generally illustrated as following:
(4) The application of flying saucer engine technology
One of the most remarkable application advantages of flying saucer engine technology is high speed aviation in vacuum, its significance in military affairs, outer space exploration and out galaxy exploration is self-evident. As its special engine operation mechanism ——directly activating and controlling the PNT of atomic nucleus of atom system, its accelerating function and flying speed are of course imaginable. As it accelerates by activating the atomic nucleus PNT of atom system directly, as long as atomic nucleus PNT activation negative restriction is not too rigor objectively, as long as we can do well in control of critical consistency of PNT activation orientation and critical equilibrium distribution of PNT activation strength it’s evident for us to imagine that the flying saucer engine can not fly slower than the similar particles accelerated in high-energy accelerator, and even, as the remarkable advantage of direct atomic nucleus PNT activation relative to the electromagnetic alternate acceleration of high-energy accelerator, the flying saucer engine can fly much more easily and faster and similar particles in common high-energy accelerator.
In military affairs, as flying speed and acceleration function of flying saucer engine is rather remarkable, the variation of the positive and negative mass quotient K is consequently remarkable, as a result, flying saucer engine is not convenient to tote any routine weapons like missile series, and in fact, missile series can not match flying saucer engine. As its connatural resource advantage of atomic nucleus PNT activation, flying saucer engine is rather convenient to scheme laser weapon with super orientation, high speed, powerful execution, or similar weapon of high speed particles.
Of course, the application of flying saucer engine technology does not limit in aviation, in fact, flying saucer engine technology itself is just out-and-out high quality nuclear energy technology, and we can of course design and fabricate low intensity flying saucer engine as train engine; and because electrical power has advantage of being convenient to transmit and disperse using, we can of course design and fabricate flying saucer engine generator, … …。
Meanwhile, because the facilities as flying saucer train engine and flying saucer engine generator directly work outside, during the course of the practical usage, it is necessary to renew or supply the proper flying saucer activation source material periodically, which is similar to that any nuclear power plant need renew or supply nuclear source periodically. This is much different from flying saucer engine flying in vacuum, as long as the flying saucer engine does not radiate outside, and no matter what its flying speed is or how long time it flies, the total mass and general energy of the flying saucer engine are generally conserved, this is similar as the particles or photons flying in vacuum. At the same time, the flying saucer engine generator won’t be sure to drag winding moving in magnetic field, upon the proper choice of the flying saucer engine source material and the proper PNT activation, the flying saucer engine can activate strong electric field, and produce activation current, -----PNT activated current.
But, on the other hand, flying saucer engine technology has a disconcerting reverse. As flying saucer engine technology directly works on the atomic nucleus by the connatural way to activate and control PNT of matter system, under the very technological background, building an A-bomb may be as easy as cooking a dinner. After all, compared to the flying saucer engine technology, nucleus chain reaction detonation technology but resembles one of the rough failure models of atomic nucleus PNT volitional activation. And at any rate, confronting the ballyhack capability of the potential power of cosmic matter, vitality is too frangible.
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