Коганицкий Григорий. Part Three_B_1 - Overcoming Multilevel Continental Anti-Missile Defense By Usage The Virtual Mirror Method

OVERCOMING THE CONTINENTAL MISSILE DEFENSE

All innovations declared here are the property of the author and cannot be used without his consent.

MEDIUM AND LONG RANGE TACTICAL STRIKE WEAPONS

PART ONE - CRUISE MISSILE OF VARIABLE GEOMETRY, HAVING RAMJET ENGINE WITH ADDITIONAL INJECTING/FEDDENG OF INLET AIR FLOW

http://samlib.ru/k/koganickij_g_a/turnskin_2.shtml

PART TWO - ANTI-SHIP MISSILE, HAVING RAMJET ENGINE WITH ADDITIONAL INJECTING/FEEDING OF INLET AIR FLOW

http://samlib.ru/k/koganickij_g_a/anti_ship_missile.shtml

PART THREE_A - GUIDANCE ALONG SPIRAL AND OVERCOMING MULTILEVEL ANTI-MISSILE DEFENSE

http://samlib.ru/k/koganickij_g_a/along_spiral.shtml

PART THREE_B_1 - OVERCOMING MULTILEVEL CONTINENTAL ANTI-MISSILE DEFENSE BY USAGE THE VIRTUAL MIRROR METHOD

PART THREE_B_2 OVERCOMING INSIDE THE CONTINENTAL LOCAL ANTI-MISSILE DEFENSE

PART THREE_B_3 THE VALVELESS, PULSEJET, DETONATION ENGINE DECIGNED BY A DOUBLE-LOOP CIRCUIT.

I will talk about this topic only with a specific customer and on condition of prepayment.

Generals are always prepared to fight the last war.

Words from British Prime Minister Winston Churchill

OVERCOMING THE CONTINENTAL MISSILE DEFENSE

As I wrote earlier - "I began to be interested in the topics that I will talk about - "Overcoming the continental missile defense system" and "forming a virtual mirror" back in the USSR" and At first I published such a topic in 2015

An interesting situation has arisen in modern military missile technology in the field of long-range missiles and their interception.

On the one hand, it is the complete stagnation of scientific thought and the lack of innovative ideas in the field of designing the rockets themselves - they remained at the fundamental level of the German FAU2.

This problem is very old and comes from the ideology and specificity of "American" military technical thought, which, having lost its competitor such as the USSR, degraded to the level of a banal sharing out of taxpayers' money.

On the other hand, electronics and control systems have developed so much that even Elon Musk's water tower can fly under their control, if it be equipped with enough powerful engine.

Such multistoried "water towers", in which most of the power of the first stage engine is spent on accelerating the passive mass and the atmosphere poisoning, began and continue to be launched all over the world, with the light hand of Werner von Braun.

Why just by Werner von Braun?

After all, there were other alternative ways of developing astronautics, proposed by Tsiolkovsky and Zander.

Tsiolkovsky proposed a scheme for parallel connections of rockets, IN WHICH ALL ENGINES WORK AT THE SAME TIME, and the fuel is redistributed between the rockets and the rockets that have used up their fuel are detached and returned to the ground.

Zander developed the idea of rocket planes, in which a winged, re-entry stage, having an engine CAPABLE OF WORKING IN TWO ENVIRONMENTS, lifts a purely rocket stage into near space.

Werner von Braun, that was polished and absolutely unprincipled, who was easily swapped out badge of his Nazi Party for one of one of American's club badge, was a quite at home in US, and was quite understandable man for Americans' parvenu, which came from the midst of bootleggers and cowboys which stealing neighborhood chicken-coop.

And what about Tsiolkovsky и Zander!?

One of them is a deaf and poor unmercenary old man and the second is even worse - an ideological socialist-terrorist.

It is Impropriate, they have bad manners!!

In addition, at that time, in the short term, the purely American familiar scheme to be the most advantageous - to plunder a burning chicken coop.

After the end of the war, in which the United States entered at the final stage and fought rather mediocrely and, basically, by the hands of other nations, they seized and took away from Germany: not only patents; equipment and technical documentation, but also (С_https://www.nasa.gov/people/wernher-von-braun/) As part of a military operation called Project Paperclip, he (Werner von Braun - my comment) and an initial group of about 125 its employee were sent to America where they were being located at Fort Bliss, Texas. There they worked on rockets for the U.S. Army and assisted in V-2 launchesх at White Sands Proving Ground, New Mexico.

What is the situation in the field of rocket technology design now??

The era of the 125 rocket men who were sent to America under escort 75 years ago was ended due to natural reasons.

Russia has degraded to such level that there is nothing left to steal from it - there are no creative ideas or competent people there.

Scientists from developing countries are sought after at home and quite successfully find well-paid and interesting jobs there.

The level of education and mentality in the United States produces people who are not interested in anything other than alcohol, drugs and computer games.

Moreover, the most "creative" of them are only capable, following the example of the Great Rocketeer certain Matt Walker from the Air breathing Propulsion division at NAWCWD of Lockheed Martin, to steal someone else's intellectual property from the Internet and then modestly hide in a corner, like that innocent girl, who became pregnant while working as a prostitute and now hopes that its paunch resolving itself.

THIS IS VAIN HOPE - IN SUCH MANNER THIS IS NOT BE RESOLVING.

So, what is the current situation in the field of preparations for the "doomsday" war?

As I said above: "all advertising statements and hopes revolve around the expectation - all of that will be resolving itself"

Let's first consider a quite low-cost and low-tech way to overcome the modern, or, more precisely, the most advertised continental missile defense system.

In part THREE_B_1 I want to examine theme "OVERCOMING MULTILEVEL continental missile defense by USAGE OF THE VIRTUAL MIRROR METHOD"

The missile defense breakthrough scheme I propose is based on three VERY old ideas:

Tsiolkovsky's ideas - about the parallel operation of unified rockets as part of a rocket train;

Zander's ideas - about launching a payload into orbit using a rocket-plane with an engine capable of operating in two environments;

And the ideas of Dr. Eugen Senger in collaboration with mathematician Irena Bredt - Antipodal-Bomber.

To which I added my own idea - "formation of a virtual mirror covering a missiles' orbital attack".

Of course, the ideas of the apostles of rocketry have been reworked by me to suit modern materials and a modern understanding of the problems in which faced rocket flying at the stratosphere.

So - OVERCOMING THE CONTINENTAL MULTILEVEL ANTI-MISSILE DEFENSE

What is needed to guarantee overcoming the currently existing, multi-level, having satellite support, but rather primitive continental anti-missile defense?

It is necessary to ensure RADAR AND OPTICAL INVISIBILITY of penetrating warheads throughout the entire stratospheric segment of their movement in the anti-missile defense coverage area.

It is necessary to provide the opportunity, from ANY arbitrarily chosen starting point, to hit ANY selected point on the earth's surface.

Warheads must have the ability to actively maneuver at ANY point of their trajectory, including side-sliding - all of that makes their ballistic interception impossible.

At the last stage of the trajectory, when they passing the short-range anti-missile defense, the warheads MUST GENERATE SUCH A NUMBER OF FALSE TARGETS, which will bring the anti-missile defense system into a state of time trouble.

At the last stage of the trajectory, when passing close anti-missile defense, warheads must be able, if necessary, WORKING IN A GROUP, to evade physical interception and redistribute targets within the group.

The basis of the strike missile system is a missile train (hereinafter the term will be used - a modular missile), made according to a series-parallel scheme from separate, unified and partially autonomous modules, capable of acting as a united structure before of its entering in the trajectory of overcoming air defense.

Each autonomous module is designed as a radial (120*) section of a figure of revolution. A detachable a center wing section with auxiliary load-bearing planes is installed between the active modules.

Each modular rocket consists of seven sub-modules - three rocket modules; a center wing section and of three fuel tanks.

Each sub-module designed as a complete and autonomous design that has both its own functionality and is capable to work in cooperation with other modules to fulfill the main task - breaking through continental anti-missile defense.

The anti-missile defense breakthrough complex is launched into the stratosphere as part of a rocket train - a carrier rocket plane, based on a modified Su27 aircraft and a modular rocket.

Such a rocket complex, until the moment of decoupling, should be able, acting as a united system, to be arise at supersonic speed to an altitude of 35-40 km, using SIMULTANEOUSLY all its engines and constantly replenishing the modular rockets' fuel tanks.

The fuel for the modular rocket is aviation kerosene, and the second component is hydrogen peroxide.

At the initial stage of entering on the orbital trajectory, both fuel components come from the main and external tanks of the carrier aircraft.

After completing the initial stage of entering the orbital trajectory, the modular rocket separates from the carrier aircraft and begins to accelerate to orbital speed.

The carrier aircraft returns to the base airfield.

Up to moment of entering on the orbital trajectory and decoupling the sub modules, fuel for its' engines comes from the sub modules of the fuel tank located in front.

After entering on a low-orbit trajectory, for: transition of rocket sub modules to a trajectory of ricochet; to overcome the border of long-range continental anti-missile defense or when there is a danger of interception - the modular missile is divided into separate sub-modules.

To performing maneuvers of: missile module entering into ricochet trajectories; to evade from interceptor missiles and accurately guidance to a target - fuel from the missile module tanks is used.

Why was Su27 chosen as the basis for the rocket-plane?

Today it is the most widespread and relatively cheap supersonic fighter capable to flying in the stratosphere.

What modifications are required for Su27 to ensure that the rocket complex rises into the stratosphere to the altitude necessary to prepare for a missile defense breakthrough?

Since the carrier aircraft enters the stratosphere, where aerodynamic rudders are ineffective, after separating the rocket modules which are stabilized the ENTIRE missile complex with their gyroscopes, in order to avoid from stalling the carrier aircraft into an abnormal flight mode, it is necessary to install into carrier-aircraft, its own three-coordinate power gyroscope.

Since the engine of the base Su27 is not designed for flight at altitudes above 18,000 meters, the afterburner in the carrier-aircraft is upgraded to the level of a dual-medium engine capable of providing operating thrust to altitudes of at least 30,000m.

For such modernization, the Su27, AL-31F engine has a sufficient level of double-looping.

For satellite surveillance, the appearance of the aircraft does not change with such modernization.

The figure shows below one of the options for upgrading of the afterburner based on my earlier published work.

http://samlib.ru/k/koganickij_g_a/overcoming_1.shtml (Posted: 16/10/2011),

1 - toroidal generator-injector of a vapor-gas mixture (feeding systems and catalyst plates are not shown in this figure); 2 - toroidal torch of vapor-gas mixture; 3 - air/exhaust gaz supply from a turbojet engine (swirler is not shown in this figure); 4 - vortex formation zone (swirler and fuel torch formers are not shown in this figure); 5 - zone of vortex DETONATION combustion; 6 - adjustable nozzle

More modern publication - http://samlib.ru/k/koganickij_g_a/turnskin_2.shtml (Posted: 03/12/2023)

8 - catalyst plates; 9 - supply of hydrogen peroxide; 10 - perforation of the fire chamber; 11 - fuel supply

Targeting and maneuvers are carried out, depending on the height, either due to the asymmetric flow of the incoming airflow around the missile modules or through the ASSYMMETRICAL RICOCHET of the missile modules from the dense layers of the atmosphere.

The rocket modules have an aerodynamically asymmetrical body, which has a fairly high aerodynamic quality and low lateral stability.

The movement of rocket modules upon entry into the atmosphere or local turbulence is reminiscent of entering a transverse wave of a boat with a redan and a deep V bottom.

More earlier publication -http://samlib.ru/img/k/koganickij_g_a/overcoming_1/overcoming_1-17.jpg (Posted: 16/10/2011),

1 - module incoming in the dense layers of the stratosphere; 2 - module that performs ricochet; 3,4 - module on the active acceleration trajectory after a ricochet; B - proposed air flow pattern

By choosing the pitch angle and the required heading angle, the rocket module creates an asymmetrical vortex zone on its lower surface.

A change in the position of the axis of the rocket module relative to the axis of movement, a change in the relative positions of the center of gravity and the center of pressure, or a transverse tilt of the body relative to the plane of movement causes lateral sliding and a change in the direction of movement.

Due to the lack of a special term, I conventionally called this mode of movement as sliding.

The sliding mode is used to: perform ricochet, guidance and/or anti-missile maneuver from the moment the missile module enters the dense layers of the atmosphere.

It is assumed that it is possible to use a sliding mode on an arbitrary section of the trajectory for an anti-missile maneuver at the moment when the action of the anti-missile system is detected (1-7-B).

The control elements of the gliding missile module is a rotating warhead that changes its own position inside the aero-carrying body and a compensating ring or auxiliary gyroscope.

It is possible to use a warhead of both conventional and nuclear types.

I have developed concept of a 30-50 kiloton nuclear warhead, which can be rotated at high speed, having a hypothetically high ratio of usage of fission material and can be produced from a non-weapon's plutonium and by simplified technology.

But, I will talk about this topic only with a specific customer authorized by its State and on condition of prepayment.

The rocket modules moves along a wave-like trajectory, carrying out ricochet from the atmosphere according to the method proposed by Dr. Eugen Senger in its work - Antipodal-Bomber

After separation, the fuel sub modules continue to move along a low-orbit trajectory.

The flight of fuel sub modules is not stabilized in space and they randomly somersault on a low orbital trajectory, ahead of rocket sub modules.

In a step's part of each fuel sub module, several short mortars designed to shoot pirocartriges containing sodium are installed.

Pirocartriges are fired sequentially and in a random direction, with individual delays set by electrochemical timers which should be initialized in the moment when the fuel sub modules are separated.

Fuel sub modules do not have their own electronic control or communications systems, and each mortar with pirocartriges is simply a piece of pipe with a sodium charge and electrochemical timers cocked at the moment of separation.

As a result of using such a scheme, even the complete destruction of the module by ballistic interception does not affected at the performance of its main function - shooting out sodium pirocartriges during of the flight along trajectory.

Why needing to fire out sodium pirocartriges along the flight trajectory?

In the stratosphere, the near-Earth plasma is in a metastable state, so any impact on it acts as an "instability trigger" and leads to the occurrence of "auroral phenomena."

According to the results of numerous scientific experiments, one of such effects is the spraying of superheated sodium vapor into the stratosphere.

Ionized particles present in the upper atmosphere during auroras interfere with the propagation of radio waves, causing signals to scatter and weaken. This phenomenon is known as auroral absorption.

Aurora changes the specific shape and appearance of both the transmitted and received radio signals - the signal is received as noise fenomenon. This noise is caused by the Doppler effect, and look like as chaotic noise.

The release and spraying of vaporized sodium metal into the stratosphere creates critically affects for radio communications and radars, such influence equivalent to the effect of a powerful solar flare aimed at the earth or a thermonuclear explosion in the stratosphere

The combined optical and radio impact on both satellite and ground-based surveillance and reconnaissance facilities, through the Aurora, artificially created along the trajectory of the modules, includes, among other things, disruption of operational radio communications.

Such combined impact will disorient the continental multilevel anti-missile defense system and make missile modules moving at the boundary of the stratosphere along a multiple ricochet trajectory completely invisible to it.

HOW IS CARRIED OUT BREAKING THROUGH A SHORT-RANGE CONTINENTAL AIR DEFENSE AND ACCURATELY TARGETING TO SPECIFIC OBJECT.

Taking advantage of the fact that missile modules are able to move outside the ballistic trajectory and perform sideways sliding, they are able to attacking a target from several directions, moving in a downward spiral.

The exit of rocket modules from under the auroral canopy will, as I assume, occur at an altitude of about 30-40 km.

For a missile module moving by spiral with a reduced rate of descent of more than 3 M, this corresponds to being in the possible interception zone for approximately from 40 seconds to one minute.

This method of organizing a breakthrough of the near air defense zone is described in sufficient detail in the chapter - PART THREE_A - GUIDANCE ALONG SPIRAL AND OVERCOMING MULTILEVEL MISSILE DEFENSE

http://samlib.ru/k/koganickij_g_a/along_spiral.shtml

In addition to this, when "the missile modules which has ability of maneuvering and redistributing target inside group" are used for overcome a missile defense, it has another possibility in which the missile modules themselves, without of usage of smart "jammer," are capable to suppressing the missile defense detection and guidance system in targeted mode.

Moreover, to control this function, they do not require extremely high-speed computers and complex control units.

I conventionally called this method the "slipping radio mirror method"

The figure below shows one of the options for implementing this method of overcoming missile defense based on my earlier published work.

http://samlib.ru/k/koganickij_g_a/overcoming_1.shtml (Posted: 16/10/2011),

http://samlib.ru/k/koganickij_g_a/overcoming_2.shtml (Posted: 18/10/2011),

The missile module does not have a smart unit of jamming.

In the simplest case, this is a traveling wave tube, the control of which is cooperated with unit of the targets redistribution by method described in previous articles.

The missile module having caught the enemy missile defense radar signal, with a short time delay, simply re-radiates it to other missile modules of its group, and they, without any signal changes, radiate it into the front hemisphere, influencing the side lobes of the radar's antenna diagram.

Since the signal speed is much higher than the scanning speed, but is finite, the operator/computer sees not one, but at least three, closely spaced real targets.

Moreover, since the missile modules maneuver and their positions relative to one another are constantly changing (the distance and, accordingly, the time of passage of the signal between them changes), the positions of these virtual targets also do not statistically repeat their prototype, but carry out independent, real maneuvers.

Since every missile sub module operates this way, in the event of a breakthrough of the missile defense system by three sub modules, the operator/computer sees at least nine real targets. And in the event of a breakthrough by three modular missiles, divided into nine sub-modules, missile defense operators see at least eighty-one maneuvering targets.

That is, when the number of missile sub-modules increases above some terminal limit, in order to search for real targets and generate commands for interceptor missiles, computer speed will be required an order on level higher than it is achievable in currently level.

I have also developed A CONCEPT FOR DETECTING AND TRACING OUT MISSILE MODULES THAT BREAK THROUGH THE CONTINENTAL MISSILE DEFENSE SYSTEM UNDER COVER OF THE AURORA'S CANOPY by multiple ricochet mode according to the scheme described above, but I will talk about this topic only with a specific customer and on condition of prepayment.

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Аннотация: What is the situation in the field of rocket technology design now?? The era of the 125 rocket men who were sent to America under escort 75 years ago was ended due to natural reasons. Russia has degraded to such level that there is nothing left to steal from it - there are no creative ideas or competent people there. Scientists from developing countries are sought after at home and quite successfully find well-paid and interesting jobs there. The level of education and mentality in the United States produces people who are not interested in anything other than alcohol, drugs and computer games.

Коганицкий Григорий : другие произведения.

Part Three_B_1 - Overcoming Multilevel Continental Anti-Missile Defense By Usage The Virtual Mirror Method