WO2022259138A1

WO2022259138A1 - Closed circuit space shuttle (in which no water, hydrogen or oxygen is lost)

Info

Publication number: WO2022259138A1
Application number: PCT/IB2022/055282
Authority: WO
Inventors: Petrica Lucian GEORGESCU
Original assignee: Georgescu Petrica Lucian
Priority date: 2021-06-08
Filing date: 2022-06-07
Publication date: 2022-12-15
Also published as: RO135272A0

Abstract

The invention relates to a closed-circuit space shuttle used for interplanetary and interstellar transport and to capturing solar energy, being a constructive combination between rocket and aircraft in which the take-off and landing are made vertically, and the vertical take-off does not last more than a minute, after which the space shuttle is driven like an airplane using the load-bearing force generated by the 9 wings that support the four rockets of the space shuttle, the airplane regime being possible due to the atmosphere of the planet in which it is, excepting only the Earth satellite which has a gravity of 0.17 G, but has no atmosphere, for the correct operation of the shuttle its acceleration must be greater than 0.1 G, and 1G being the gravity of the Earth. The shuttle, according to the invention, is powered only from the outside with only solar energy and energy from laser cannons, being recommended to use laser cannons or thousands of mirrors that focus the sun's rays during takeoff until the exit into outer space on the shuttle, which together with the friction will heat the outer surface of the space shuttle and for a homogeneous heating of the entire surface of the shuttle must rotate around its axis two or three times a minute, use laser cannons during takeoff until the exit in space, giving the possibility to reduce the amount of fuel on board the ship which will be 20 times smaller to put the shuttle in space on our planet, the propulsion system being made by 19 double rocket engines, (ie rocket in rocket). The inner rocket works by burning hydrogen and oxygen, and the outer rocket concentrically is fed by high pressure steam that washes the inner rocket accumulating an even higher thermal energy, respectively, kinetic, the shuttle has four more rockets, having a total of 76 double rocket engines.

Description

Closed circuit space shuttle (in which no water, hvdroqen or oxycien is lost)

(I) THE DESCRIPTION.

The invention relates to a new closed-loop propulsion concept for space shuttles (ie no drop of water, hydrogen, or oxygen is lost). This very complex invention can be used in all types of transport, especially in interplanetary and interstellar transport. This space shuttle is a constructive combination between the rocket and the plane in which the takeoff and landing are done vertically. The load generated by the 9 wings that support the four space shuttle rockets, the space shuttle flight regime is possible due to the atmosphere of the planet it is on, except for the Earth satellite (it has no atmosphere, but is not a problem because gravity of The Moon is 0.17 G.). For the proper functioning of the space shuttle, it is necessary that during the whole transport, the acceleration of the space shuttle must be greater than 0.1G (1G is the Earth's Gravity), so we must have a continuous acceleration that will never exceed 1G and travel time will be greatly reduced. Due to this acceleration, the life of the astronauts on board the space shuttle continues to be greatly improved and the astronauts no longer live in weightlessness. Moreover, astronauts are also protected from solar and cosmic radiation due to water and steam tanks from the outer extremity of rockets and wings on the entire outer surface that take this energy from solar and cosmic radiation due to water and steam tanks from the outer extremity of rockets and wings on the entire outer surface that take this energy from the sun and cosmic radiation and together with the energy given by friction, the outer walls of the rockets and wings, will heat up, heating the water into steam, steam that is used to propel the space shuttle or rotate the toroidal vertical engines with turbines in number of 72 pieces (ie 12 vertically and 6 horizontally in each rocket), which drives direct current electric generators, supplying direct electricity to the entire space shuttle system, but especially the electrolysis system. The hydrogen and oxygen supply of the space shuttle will never be made from outside. The space shuttle will be powered from the outside only by solar energy, and energy from laser cannons (technology we currently have on some American warships) and of course from thousands of mirrors that focus the sun's rays on the shuttle. It is recommended that the use of laser cannons, which together with the friction will heat the outer surface of the space shuttle, during takeoff into outer space, and for a homogeneous heating of the entire surface of the space shuttle must rotate about its axis of two or three times a minute. The use of laser cannons during takeoff until the exit into space, allows the reduction of the amount of fuel on board the space shuttle, to be 20 times smaller for placing space shuttles in space on our planet. The propulsion system is made up of 19 double rocket engines (ie rocket to rocket, where the internal rocket engine works by burning hydrogen and oxygen and the concentric rocket engine to the first, is powered by high pressure steam that washes the inner rocket accumulating even more energy thermal and kinetic). The space shuttle has four rockets with a total of 76 twin-propulsion rocket engines. The 19 double rocket engines on each body are located at the top of the fire cylinder, so the center of gravity of the rocket or space shuttle is under the propulsion system, thus having a much greater maneuverability and forward direction control. If the space shuttle moves, ie. from Bucharest to Tokyo, the energy consumed to reach space is recovered by the Sun and especially by the friction of the space shuttle with the atmosphere, which will heat the outer surface of the space shuttle, this makes water to be overheated generating steam for propellants, for better maneuverability and especially for driving vertical toroidal motors with turbines that take the kinetic thermal energy of the steam from the fire cylinder, driving the electric generators of direct current (we do not need electric batteries space shuttle) so that much of this electricity will be used to power the electrolysis plant, generating oxygen and hydrogen so that the high pressure toroidal tanks will be refilled with hydrogen and oxygen, so after landing the spacecraft is ready to takeoff. The maneuverability of advancing the Space Shuttle is done with the help of tubes with two rocket engine systems in opposition, these tubes are placed above the landing system in the three outer rockets perpendicular to the radius of the central rocket resulting in the rotational movement of the space shuttle. The lower part of the steering wheel is made by the two cylinders with opposing rocket engines, located in the central rocket, one tube above the landing system and the other tube below the control system and the cargo area of the central rocket. Depending on the applicability, this invention can be built from 1 m long to several hundred meters long (in outer space). It can also be used to capture solar energy. With hundreds of mirrors around the space shuttle hundreds of meters in radius, the mirrors focus the sun's rays on the black space shuttle (or rather focus on the 4 rockets and 9 rocket support wings. The space shuttle can have a single rocket). , two, three, four, or more rockets, for this invention we chose a space shuttle with four rockets, one inside three outside, all the rockets are supported by the 9 wings and we will have a rocket in the center and three In this space shuttle we do NOT need electric batteries, because the electricity is produced in this space shuttle by its own operation, and the electricity that is not used during the day will supply electricity to the system with direct current of electrolysis generating hydrogen and oxygen, which can be used during the night or in the moments of extra consumption of electricity during the day, or to have a direct supply of direct current electricity to the electrolysis system for the preparation of the space shuttle to take off. The double rocket engine (rocket to rocket) is located at the top inside the rocket in the central fire tube in 19 pieces in number under the steam supply, which is pressurized by the steam turbines, each steam turbine is operated independently of an electric motor of direct current, and directed in the cylinder of each engine- double-rocket, so the steam is depressurized in the area of cylinder 3 water and steam in the immediate vicinity of the fire cylinder and in the area of cylinder 1 of water and steam outside, inside the rocket pressurized by steam turbines (which can be two, four, six or eight in number

. ) in this invention I chose two turbines for steam pressurization, one turbine rotates in one direction and the other in one direction opposite. The electric motors of these turbines will be powered by approximately the same electric power (so the turbine below will have a higher rotation) so that the pressurized steam is overheated by washing the rocket engine which works by burning hydrogen and oxygen and by washing the support fins of the rocket engine that runs on hydrogen and oxygen, of the cylinder of each double rocket engine and of course of the fins inside the cylinder of the double rocket engine. Inside the fins are mounted electric heaters powered by direct current for even greater heating of the superheated pressurized steam, which are mounted all around the entire length of the cylinder of the rocket engine that runs on hydrogen and oxygen. So the double rocket engine is the campus of two rockets (rocket in the rocket), the central rocket engine that works by burning hydrogen oxygen, and the outer rocket engine in which the pressurized steam washes the inner rocket engine that works by burning hydrogen and oxygen, and all the fins from inside the engine cylinder double rocket. Hydrogen oxygen is supplied by supply turbines driven by direct current electric motors, the supply being made from high pressure horizontal toroidal tanks. The high pressure horizontal toroidal tanks have the rocket in the middle of the central rocket shuttle are oxygen The horizontal high pressure toroidal tanks of the three outer rockets are hydrogen (to greatly reduce the possibility of an explosion because the high pressure toroidal tanks are hydrogen and oxygen long distance from each other and in different rockets). In the rocket can be mounted: a single double rocket engine, seven double rocket engines (one in the center and six around), or 19 double rocket engines as in this invention, or several double rocket engines depending on the size of the rocket and the size of the double engine rocket. In this invention we have 19 double rocket engines in each rocket, so the space shuttle of this invention having 4 rocket tubes will have a total of 76 double rocket engines. As can be seen, we have two propulsion systems, one by burning hydrogen and oxygen, and the other propulsion by superheated pressurized steam. This energy of superheated pressurized steam together with the energy of gases generated by the combustion of hydrogen and oxygen (resulting in water vapor having a kinetic energy and temperature much higher than superheated pressurized steam) which are introduced into the central fire tube at a very high speed high and a very high temperature, the rocket effect causes the space shuttle to move in the opposite direction to the displacement of the flue gas (resulting in water vapor) of the superheated pressurized steam. Part of this thermal energy that is introduced into the fire cylinder is taken over by the heat transfer fins which also have the role of mechanical support of the fire cylinder, the water and steam cylinder, and the thermal insulation cylinder. These fins are mounted in the fire cylinder (near the propulsion system of the 19 double rocket engines close to the base of the fire cylinder) from the area of the horizontal toroidal tanks to the base of the fire cylinder, ie in the area of vertical toroidal engines for capturing heat and the kinetics of the propulsion steam, these heat capture fins are in number of hundreds of pieces placed around the inner cylinder of the fire and on the entire height of this fire cylinder, transfer fins take heat from inside the fire cylinder generating steam of a very high temperature and pressure, steam that is introduced into the area of cylinder 1 inside water and steam, the fins are supplied with water from the area of vertical toroidal motors so that the water introduced with pressure at a temperature of 10 degrees Celsius, which will wash the entire outer part of the inside of the heat transfer fins generating steam at a very high pressure temperature (inside the fire cylinder near the propulsion rockets have a temperature of over 3000 degrees Celsius and due to these fins and toroidal vertical transfer motors, all thermal and kinetic energy is taken over so that at the bottom of the fire cylinder the temperature will reach below 80 degrees Celsius and a very low pressure close to 0.7 atmospheres) so the propulsion steam will not reach the bottom of the fire cylinder and will not put no pressure on the bottom of the fire cylinder, so the rocket will not be braked. The steam that is introduced from the fins into the inner cylinder 3 of water and steam, although the steam is introduced at a very high temperature and pressure, the pressure in this inner cylinder 3 of water and steam never reaches more than 1.5 bar Thanks to the independently operated steam turbines, each turbine is powered by a direct current electric motor, taking this pressure from this inner cylinder of water and steam, in which the steam is depressurized and pressurized in the 19 cylinders of each double rocket engine. This thermal energy taken up by these "minus" heat transfer fins rubbing the propulsion steam by the heat transfer fins and rubbing against the wall of the fire cylinder is the force with which the space shuttle is pushed. The other part of the remaining energy, thermal and kinetic steam, is taken up by the 72 vertical toroidal motors (which operate in turbine style and with a rocket effect) where this energy is largely converted into electricity by direct current electric generators, and it also helps to recover and re-circulate steam water. The rocket has 72 vertical toroidal heat transfer motors mounted in 6 columns and in 12 rows. All turbines of these vertical toroidal motors have the same rotational speed, this synchronization is done by the gears that are driven by the toothed crown of the turbine disc of the vertical toroidal motor, and the vertical toroidal motors are located on the six columns of the rocket, having 11 wheels toothed on the column for the synchronization of the 12 turbines of the vertical toroidal motors that capture the thermal energy of the propulsion steam and the kinetic energy of the propulsion steam from the fire cylinder, the synchronization of the rotation speed continuous which are mounted horizontally synchronizing the 6 columns of the turbines of the vertical toroidal motors. DC electric generators can be 36 pieces in the racket, so 6 generators serve 12 vertical toroidal motors (ie six columns and two rows) or we can have in the racket 18 direct current generators, each 6 generators DC serve 24 vertical toroidal motors (ie six columns and four rows) or we can have in the rocket 12 DC generators, in which each group of 6 DC generators can serve a group of 36 vertical toroidal heat transfer motors (ie six columns and six rows) or we can have only six direct current generators inside the rocket serving all the turbine turbines inside the rocket being mounted in the middle of the front 36 vertical toroidal heat transfer motors above and 36 vertical toroidal heat transfer motors below the direct current generators . So all turbines of vertical toroidal heat transfer engines take over the rest of the kinetic and thermal energy of the propulsion steam, the energy left untaken by the heat transfer fins, the heat and kinetic energy absorbed from the fire tube in each turbine of the toroidal engines, is approximately constant, the received energy adjustment being made by opening more or less the steam inlet inside the vertical toroidal motors in the fire cylinder. Exceptions are the last rows of vertical toroidal heat transfer motors, especially the last two rows of vertical toroidal motors, which even if they have the maximum open intake will take over some of the mechanical energy of the other toroidal motors above them. Or rather, these last two rows of 12-piece vertical toroidal engines (ie 6 columns and 2 rows) will depressurize the remaining steam pressure at the bottom of the fire cylinder, the pressure of this water vapor will reach below 0, 7 bar and a substantial drop in temperature. So the propulsion steam will not put pressure on the bottom of the fire cylinder (the rocket will not be braked). So the space shuttle has 6 columns and 12 rows of vertical toroidal motors. The steam intake in the vertical toroidal motors is made by two columns that follow the round shape of the vertical toroidal motor and enter the toroidal motor from 300 degrees to 120 degrees from the outer length of the vertical toroidal motor. So along this length the outer part of the vertical toroidal motor is missing, to allow steam to enter the turbines inside the vertical toroidal motors. Tapered tubes that take the propulsion steam from the fire cylinder and direct it into the inlet area outside the vertical toroidal engine, the area that is open 180 degrees to hit the turbine blades, the direction of rotation of the turbine inside the engine vertical toroidal, will be in the direction of movement of the incoming steam. The steam will hit the turbine blades hard and will be further forced and pressurized and directed through 6 tapered holes (of each turbine blade) to increase the speed of the larger blade inside the rotor which will be tangent to its rotational motion, increasing - and even more the mechanical rotating force of the turbine using the rocket effect, this effect further increases the power of the turbine inside the vertical toroidal motor. The toothed crown on the outside of the turbine disc drives the top gear and the bottom gear, driving the vertical toroidal turbine sprocket at the top and the vertical toroidal turbine sprocket at the bottom. Thus, all the turbines on the column are kept at a constant speed, and due to the coupling of the direct current generators, all the turbines of the vertical toroidal motors with rocket turbines have the same rotation speed. Because the speed and temperature of the propulsion steam in the fire tube decreases (from the top of the propulsion level of the 19 double rockets to the base of the fire cylinder), and to maintain the approximate power on each turbine in the rocket, all having the same The intake of the steam from the fire tube regulates the intake, opening more or less the entrance of the propulsion steam in each vertical toroidal engine, thus having an approximately equal power in all the toroidal engines in the rocket. So the electricity generated by these DC generators driven by the 72 turbines of the vertical toroidal motors, supplies the following electricity with direct current: The water electrolysis tank, the water heaters and the heaters inside the fins in the 19 cylinders of the double rocket propulsion system, of the direct current motors, of the oxygen and hydrogen supply turbines, of the direct current motors, of the steam pressurizing turbines, of the electro pumps of the water transfer recovered from the steam, of electro water supply pumps (about 10 degrees Celsius) heat transfer fins, pneumatic landing system, water cooling system that supplies all heat transfer fins, air conditioning system, electric pumps high pressure hydrogen and oxygen, and the electronic space shuttle system. So we don't need electric batteries. The space shuttle can only function properly if the gravitational force exerted on the space shuttle is at least 0.1 G (Micro Gravity). So throughout the space shuttle we have an increase in speed all the time and it is between 0.1 G (Micro gravity) and 1 G (gravitational force on earth). This considerable advantage improves the life of cosmonauts aboard the spaceship, who no longer live in weightlessness and of course any citizen of this planet can be a cosmonaut not being large variations of speed, only during the entry into a very rarefied atmosphere of a planet (has space shuttle braking) when rubbing against the planet's atmosphere, but will not be higher than 2G, and will never be exceeded. Due to the constant increase in the speed of the space shuttle, the travel time of the space shuttle to the destination will be greatly reduced. Another considerable advantage is that the area of water and steam between the outer walls of the rocket and the 1st cylinder of thermal insulation and the water walls at the top of the rocket protects from cosmic radiation and solar radiation on cosmonauts aboard the space shuttle. . Moreover, even the energy of cosmic and solar radiation, together with the friction of the outer walls of the space shuttle with the planet's atmosphere, heats the walls of the space shuttle by heating water, generating steam in the outer area inside the rocket. Another great advantage of this space shuttle is that during takeoff from Earth the space shuttle can be thermally assisted by special laser installations to heat the ship, and to focus on the entire surface of the space shuttle, the laser does not have to be focused in -one point (this is very dangerous). This energy received by laser systems could cause the space shuttle to need 20 times less fuel and oxygen to reach outer space. We have this technology and in the near future it will be very cheap and easy to use. A very important thing to do only once before the first launch of the space shuttle is to depressurize several times, and repressurize with oxygen the entire empty space in the rocket, so that ordinary air is replaced only by oxygen that will It remains at a pressure of approximately 0.6 bar inside the space shuttles, eliminating any combination of hydrogen and oxygen with other elements. Only the inner area of the horizontal toroidal tanks intended for hydrogen (which is an exception) will be hydrogen only, completely eliminating the usual air. Another important thing is that the water is well distilled and even filtered before being introduced into the space shuttle, the oxygen and hydrogen supply of the space shuttle will NEVER be done from outside the space shuttle, and will only be done with the help of energy Sunbathe, so that hundreds of mirrors placed around the space shuttle hundreds of meters away, the mirrors focus the sun's rays on the space shuttle, which is black, due to the rocket's conversion systems will eventually result in electricity which will be largely used to supply direct current to the toroidal electrolysis cylinder and high pressure electric pumps for loading horizontal toroidal tanks with hydrogen and oxygen (never use liquefied hydrogen or liquefied oxygen). From the electrolysis system, the toroidal electrolysis cylinder located at the top above the high-pressure horizontal hydrogen toroidal tanks of the three outer rockets and above the high-pressure horizontal rocket horizontal toroidal tanks of the rocket in the center of the space shuttle, all these tanks are at the same level as the propulsion system. Indeed, the supply will take several months to fill the horizontal toroidal tanks with hydrogen and pressurized oxygen at very high pressure, but this supply will only be once in the life of the space shuttle, because the return to any planet with the atmosphere energy is taken. Cosmic Radiation from Solar Radiation and from frictional space shuttles with the planet's atmosphere during the arrival of the planet, due to this great advantage the space shuttle will land on any planet with the atmosphere, almost recharged and ready to take off.

As an example take:

"Interplanetary transport”: If we have to move to Mars. After leaving the Earth's outer space, the shuttle will head for the sun for a few weeks, so the space shuttle will rotate around the imaginary axis directed directly at the center of the sun, so that the space shuttle's axis will be almost perpendicular to the sun's rays the possibility that a larger surface of the space shuttle will be exposed to sunlight and also the space shuttle will have a rotation around its axis, the rotation will be about three rotations per minute so that the shuttle will heat evenly over the entire surface. This heating of the shuttle leads to the heating of the water and to the production of steam from the area of the outer cylinder inside the rocket and the outer area of the support wings of the rockets. This steam will be depressurized from the outer steam and water area of cylinder 3 pressurized by the steam turbines and forced to pass through the Cylinder of each Double Rocket Engine. The passage of steam through these cylinders will be further accelerated because around the cylinders are fins that have inside them electric heating elements of steam heating, these electrical resistances are located in the support fins and the fins around the support cylinder of the rocket engine. These fins are constructed in such a way that the steam resulting from the propulsion has a minimum friction with these fins. The electric steam heaters in the rocket-propelled fins that run on oxygen and hydrogen will be powered by electricity all the time, but especially when the entire propulsion system will run on steam only. The electric steam heating elements mounted in the fins which are mounted all around the entire length of the propulsion system cylinder and can be supplied throughout the operation, further increasing the temperature of the superheated pressurized steam generating an even higher kinetic and thermal energy superheated pressurized steam propulsion, it should be noted that the propulsion system will never be stopped (only in case of failure) can operate from 5% to 100% of the rated power of the propulsion system, only in special cases of strict necessity in the short term, the rated power of the propulsion system can increase up to 150% but in a very short time. After a substantial increase in speed, and the full loading of the horizontal toroidal tanks of oxygen and hydrogen, the space shuttle will move to Mars, the space shuttle will begin to rotate around the axis of travel to the North of Mars and due to the continuous increase in speed. The radius of rotation of the space shuttle around the imaginary axis of direction, the radius will increase to tens of thousands of kilometers. If the space shuttle rotates perpendicular to the direction of travel, the proximity to Mars will be the same as when it began to move in the direction of Mars, and if the space shuttle rotates 90 degrees in the direction of Mars, it will result results in a constant speed approaching Mars (even if we have a continuous increase in speed) in the direction of travel and will be 120 degrees in the direction of travel, and the speed approaching Mars will increase again if the rotation in the direction of the axis to the north of Mars will be behind it, ie 60 degrees from the direction of travel we have a decrease in the speed of approaching Mars, it will be like a screw when the speed remains constant compared to approaching the planet Mars, this imaginary screw will have a step of the imaginary screw thread. When we want to increase the speed of the approach to the planet Mars we increase the step of the imaginary screw, and if we want to decrease the speed of the movement towards the planet we decrease the step of the imaginary screw. This condition is also necessary to expose the space shuttle perpendicular to the sun's rays if the direction of travel to Mars is perpendicular to the sun's rays, the space shuttle will no longer need to rotate in the imaginary axis, and its approach speed will be higher, respectively the deceleration speed will be higher. The space shuttle will have an increase in speed between 0.1G and 1G (gravity on the ground) during this trip, this speed depends on the energy it captures from the sun's rays, so the space shuttle must move perpendicular to the sun's rays and rotate all the time around its axis with a homogeneous heating, with a greater exposure of the space shuttle to solar radiation, they will heat the space shuttle more and at the same time the water and steam that will be used for propulsion space shuttles at the same time with the continuous increase of speed and the production of electricity that feeds the entire space shuttle and especially of the electrolysis tanks, loading the toroidal tanks with Hydrogen and Pressurized Oxygen at very high pressure. This energy of hydrogen and oxygen will be used almost completely until the space shuttle reaches the very rarefied atmosphere of Mars at the top (Take the pole of Mars) but will begin to recharge from the moment it touches the planet's atmosphere. Due to the high speed of the space shuttle of over 200,000 Km / h, the speed reached during the trip, but which must start to slow down at the space shuttle almost halfway to reach the atmosphere below 50,000 Km / h, usually the devices NASA's spacecraft reaches the atmosphere of Mars at a speed of approximately 25,000 km / h, and does not recover any of this frictional energy with the atmosphere, but the space shuttle helped by the rocket effect given by the double rocket engine due to the energy of steam, steam generated by rubbing with the atmosphere of the planet Mars, the space shuttle is directed towards the center of the planet a little after moving to reduce the speed of movement so that it can remain in the very rarefied atmosphere of the planet Mars not to be rejected in outer space. The steam is formed due to the energy obtained by the friction of the space shuttle with the atmosphere of the planet Mars. As the distance begins to shrink further from Mars, the space shuttle moves in a direction perpendicular to the radius of the planet, and the braking will be done with a force of 1 G maximum 2G, and will begin to navigate around Mars , in the super-thin atmospheric space helped by the rocket effect of the propellant steam, generates a better control over the Navigation of the Space Shuttle and the distance from the planet Mars will decrease very very slowly, making 30 ... 50 rotations around the planet Mars, The deceleration force (braking) of space shuttles will never exceed 2 G (twice the gravitational force of the earth, for a comfortable life of astronauts), during which the friction with the atmosphere makes the space shuttle heats up and of course the heating of the water generates steam from the outer cylindrical tank 1 inside the rocket feeding the propulsion system and of course the production of electricity, which will be used in s especially take the electrolysis system by filling the horizontal toroidal tanks with hydrogen and oxygen. Arriving on Mars with the horizontal toroidal tanks of hydrogen and oxygen almost full.

“Interstellar transport”: After exiting into outer space, the space shuttle will head for the sun past Venus and orbit the Sun (between Venus and Mercury) for several months, perpendicular to the sun's rays for much more energy. At the same time, the space shuttle will rotate around its axis approximately one rotation per minute, even every two minutes, for a homogeneous heating of the space shuttle, during which time the speed of the space shuttle will increase. Due to this, the speed of the ship will always increase by about 1G. And due to the construction of the space shuttle surrounded by water and steam, cosmonauts will be very much protected from solar radiation so the speed will increase greatly, more than 10 percent of the speed of light, to NOT go out of orbit at the sun at this very high speed , the axis of the space shuttle will be directed a little to the sun, we stop the shuttle for a short time the shuttle will be projected tangentially in the direction of travel. It should be noted that this direction must be on the axis of movement of the sun + - 70 degrees so that the shuttle does not enter the solar system and will be directed to the nearest solar system "proxima" which is located at a distance of 4 years light so that in 40 years we can reach the nearest solar system, compared to current technology the time to the nearest solar system is several thousand years. If we consider "quantum physics" according to which in the space between planets between solar or galactic systems "is not empty and without energy" and that we have an energy fluctuation and there are several tens of hydrogen atoms per cubic meter, so using this information, the space shuttle will move perpendicular to the forward direction, rotating around the axis of movement, exposing to the maximum the surface of the space shuttle. By heating the space shuttle outside enough to accumulate an energy of growth at a speed of over 0.1G for a life as comfortable as possible for astronauts during this time, it should be mentioned that this speed and a piece of paint is catastrophic for the space shuttle. Arriving in the new solar system of course at a slightly lower speed due to the bombardment of space shuttles by hydrogen atoms (a few atoms per cubic meter), and as this speed is still too high to go to the desired planet in the new solar system, we must we orbit the new sun for several months so that we can use the energy accumulated by it so that we can brake considerably. Reaching a speed below 100,000 Km / h, and only then to go to the desired planet. Too bad our life is so short, even if we had a shuttle that could reach half the speed of lightning, it would still take us 200,000 years to cross our galaxy (the Milky Way) from side to side, or if we didn't If we were to move perpendicular to the Milky Way, it would still take several thousand years for us to be able to photograph our galaxy from one end to the other in fullness of its beauty. Space shuttle components:

Drawing No. 1 : We have the vertical section through the rocket (The four rockets of the space shuttle are identical), section no. 1 in area A, of the steering control cylinder, view of the space shuttle from the outer rocket, the next view is the view of the space shuttle from the inner rocket. The positioning of the steering control cylinders in the outer rockets are positioned perpendicular to the radius of the inner rocket, ensuring the rotation of the space shuttle. The inner rocket steering control cylinder is positioned within range, ensuring the maneuverability of the space shuttle, along with the second inner rocket steering control cylinder is mounted under the space shuttle control and cargo chamber, ensuring the maneuverability of the up and down direction, having a high maneuverability because the center of gravity of the rocket or the space shuttle is under the propulsion system.

Drawing No. 2: We have a vertical section through a rocket, Take an enlarged ladder to understand in detail all the components of the rocket.

Drawing No. 3: We have a vertical section through the rocket, section A1 from zone A, which represents the horizontal section A1 , having the following components: exterior wall, water area, walls that include thermal insulation, having the role of separating the water area and steam from the area vertical toroidal turbines, the four electric water pumps circulating in the area of vertical toroidal turbines engines in the area of cylinder 3 water and steam, the two electric water pumps circulating in the area of vertical toroidal turbines engines in the cylinder area 1 of water and steam, the horizontal toroidal system for cooling the steam from the steering control cylinder, the cooling is done by means of the internal heat transfer wings, the holes in the support plate for weight reduction, the horizontal toroidal hydro pump for circulating cold water up to the toroidal cold water tank located in the upper part of zone D, the structural role system supports you of the upper areas, steering control cylinder, turbine version.

Drawing No. 4: We have a horizontal section through the steering cylinder in zone A, with three variants of construction of the steering cylinder. The first construction is similar to the rocket propulsion system, the Micro double rocket system and micro turbines are on a much smaller scale and have only seven double rocket engines having two systems in opposition in the horizontal tube of the steering cylinder. The second construction version is equipped only with seven double rocket engines, and the third construction version with only two sets of turbines in opposition. In the atmosphere of the planet where the space shuttle is located, the double rocket system with opposing turbines must be used, and in outer space it is enough to use the set of two opposing turbines. They operate on short pulses depending on the direction of rotation or up or down direction, and operate one set of double rockets and turbines or the other set of double rockets and turbines on the opposite side. So that the steam from the horizontal toroidal system for cooling the steam is depressurized and pressurized by the two micro turbines and forced to pass through the seven double rockets that work by burning oxygen and hydrogen, this water vapor generated will have a temperature and kinetic force quite sea that will pass through the cooling wings and will be directed by the steam directing cone to the cylinder walls, in the immediate vicinity behind the opposite system of double rocket and micro turbines we have six high pressure nozzles for cold water at 60 degrees between them which will spray cold water, through a slit a spray angle of 160 degrees covering almost the entire area of the cylinder circle, greatly reducing the steam temperature and kinetic energy so that the steam will pass at a much lower speed and a much lower temperature through the horizontal toroidal cooling system where it will be further cooled, reaching again the micro system propulsion with very low energy. This difference in kinetic and thermal energy from the moment it exits the propulsion power plant until it reaches the turbines again represents the energy with which the steering tube is pushed, respectively the rocket and of course the space shuttle. If the tubes of the outer rockets receive this impulse, the space shuttle will begin to rotate if we want to rotate it in the opposite direction. If we want to change the up or down direction, the steering tube for this purpose is mounted in the central rocket with one cylinder at the base of the rocket and the second cylinder is mounted below the control chamber and the cargo space. All space shuttle steering controls are executed by these tubes with opposing Micro propulsion systems.

Drawing No. 5: We have a horizontal section through the rocket, a Mini nuclear power plant in zone 8, we have the uranium nuclear reaction control system which is surrounded by heavy water which too much thermal energy of this reaction and will be given to distilled water which will turn into high temperature and pressure steam, steam will pass through 12 pipes inside the third cylinder of water and steam heating this area of cylinder 3. The remaining steam will continue and will reach the steam pressurizing turbines in the double rocket propulsion system.

Drawing No. 6: We have a horizontal section through the rocket in the C1 area, we have the first row of vertical toroidal motors with turbines at the bottom of the rocket having the inputs permanently open at maximum in rotating mechanical energy and is taken over by direct current electric generators powering the entire electrical system of the space shuttle. In the center in the fire cylinder we have represented the cone with drops directing the steam to the maximum permissible open to the vertical toroidal motors with turbines, to avoid the braking effect that could occur by touching the inner cover of the fire cylinder by the rest of steam. We have represented the pressure adjustment tubes in the area of the toroidal motors that maintain a constant pressure adjustment of 1.2 bar, this pressure adjustment is achieved by inserting the tube more or less in the fire zone directed downwards, so that the propulsion steam will it sucks steam from the area of the vertical toroidal engines with turbines through the 12 columns. We also have represented water cylinder 3 and steam thermal insulation between cylinder number three and cylinder area 2, steam water recovery area of vertical toroidal engines with turbines, cylinder 2 steam water recovery, thermal insulation between cylinder 2 and water cylinder 1 and steam and the outer wall of the rocket.

Drawing No. 7: We have the horizontal section through the rocket in zone C2, and the vertical toroidal motors with turbines to take the kinetic and thermal energy of the steam from the fire cylinder, this energy is transformed into mechanical rotational energy and is taken over by electric generators of direct current feeding the entire electrical system of the space shuttle, we have represented the fire cylinder, we have represented the cooling fins that take the thermal energy of steam and transmit it in cylinder number three of water and steam. Water supply to big fins is made from the zone of vertical toroidal motors which has turbines, and due to the washing of the inner walls of the large fins generates steam in the area of the third cylinder of water and steam, we also have represented the pressure adjustment pipes in 12 pieces in number maintaining a pressure of approximately 1.2 bar in the area of vertical toroidal motors with turbines. We also have represented the water and steam cylinder 3 with thermal insulation between cylinder 3 and the area of cylinder 2 intended for the recovery of steam water from the area of the vertical toroidal engines with turbine and the thermal insulation between cylinder 2 and cylinder 1 of water and steam and the outer walls of the rocket. In this board we also have represented the minimum open steam intake. At the top right of the drawing number seven we have represented the large wings and the small wings in vertical section.

Drawing No. 8: We have the horizontal section through the rocket in the F1 area, we have represented the section in all 19 double propulsion rockets, the small heat take-off fins, the three-cylinder steam thermal insulation between the three steam cylinder and the 2-cylinder, and the high horizontal toroidal tanks pressure for hydrogen on rockets on the outside and oxygen on rockets on the inside. We also have a section in the connection pipe between the high pressure toroidal tanks and the thermal insulation between cylinder 2 and cylinder 1 steam and the outer wall of the rocket.

Drawing No. 9: We have represented the vertical section through the propulsion system of the 19 double rockets, in which we can see the high pressure oxygen supply and the high pressure hydrogen supply, it can be seen that the steam pressure from the pressurizing turbine, creates steam pressure in the cylinders of the double rocket of the 19 engines washing the outer casing of the rocket engine inside and the rocket support fins that run on hydrogen and oxygen.

Drawing No. 10: We have represented the horizontal section by rocket in section F2. We have represented the electrolysis system consisting of 10 concentric zones of hydrogen and alternating oxygen. The electrolysis system is permanently supplied with direct current generating oxygen and hydrogen by means of high pressure pumps. The high pressure tanks of the inner rockets are for oxygen, the high pressure tanks of the three outer rockets are for hydrogen. We also have represented the steam area pressurized by steam turbines, cylinder 3 water and steam, thermal insulation cylinder that separates cylinder 3 water and steam from cylinder 2, where the toroidal tank for electrolysis is located; we also have thermal insulation that separates the area of Electrolysis from cylinder 1 steam.

Drawing No. 11: We have represented vertical sections through the electrolysis system in zone F, and we have four drawings, drawing 1 we have represented turbine 2, driven by a direct current motor clockwise, turbine 1 driven by a direct current motor counterclockwise, turbine clamping and steam steering system, steam turbine outlet cone and a section of three twin- rocket engines with the feed system, power supply from the oxygen turbine driven by an electric motor from the turbine of hydrogen by an electric motor, both with direct current, we have represented a cylinder one steam thermal insulation that prepares the electrolysis area of cylinder 1 , steam and the outer wall, also represented is the toroidal tank for capturing hydrogen from electrolysis, and below we have the tank toroidal for capturing oxygen from electrolysis and below it we have the toroidal electrolysis system with negative bus bar, they negative electrodes and positive electrodes. In drawing number two, we have the same representation as in drawing one, in addition we have the oxygen supply tubes from the electrolysis to the toroidal capture tank. In drawing 3 we have the same representation as in drawing 1 , in addition we have a positive bus bar representation, in drawing four we have represented the same as in drawing number two in addition we have the hydrogen supply tubes of the capture tank located above the Electrolysis.

Drawing No. 12: We have represented half of the vertical toroidal turbine engine. Figure A, Represents the intake together with the intake adjustment system B, from minimum to maximum, Figure C represents the stator of the vertical toroidal turbine engine, together with the figure E of the gears, with the bars D, of the resistance of the state, Fig F represents bearings on which are mounted 2/3 in stator one third slide on the channel of the two turbines, figure G represents the cover of the turbine blades, figure H represents the blade system of the turbine, figure I represents the cylinder detachment of the blades with the steam passage holes, figure J represents the system of directing the steam towards the inside of the torus, figure K represents the cover of the turbine blades, figure L represents the water supply system from the tank ie from inside the toroidal engine to the outside, figure M represents the cooling system of the water entering the tank, figure Q represents the water tank which is fed from the outside through the hole in figure N and given to the toroidal motor through the holes of the re water tank figure N.

Drawing No. 13: We have an exploded diagram of half of a vertical toroidal motor with turbines in addition to Drawing number 12, we have figure Q of the clamping system for the intake adjustment system and figure T represents the Freon supply port of the cooling system M.

Drawing No. 14: We have represented in great detail the turbine system, together with the disc with holes and pipes and the water and steam guidance system towards the inside of the vertical toroidal turbine engine. Figure H represents the turbine blades, figure G represents the steam inlet area, figure R represents the steam steering tubes, figure J represents the water and steam guidance system inside the vertical toroidal turbine engine, figure G represents the outer cover of the turbine, figure H represents the turbine blades, figure I represents the disc where the turbine blades are located, figure T represents the inlet holes in the pipe figure R, and figure J represents the water and steam guidance system from inside the vertical toroidal turbine engine.

Drawing No. 15: We have in detail the system for collecting cold water from the tank and pressurized the outside entering through the holes of figure S. Above and below the steam pipes in figure R, Figure one represents the teeth of the crown of the inner cover of the turbines, figure L represents the slats of the water collection system from the tank and pressurized at the end, figure a represents the cold water tank figure P represents the holes in the supply tank of the L water collection system and pressurized outside. Figure V represents the freon supply port of the cooling system in figure M, figure N represents the supply port of the cold water tank.

Drawing No. 16: Represents the constructive assembly of six columns and four rows of vertical toroidal motors with turbine, figure X represents the hydro-pump, Figure W represents the cold water supply pipe from the hydro-pump, figure V represents the third cylinder of the fire zone, figure A represents the intake of the vertical toroidal motor with turbines, figure C represents the stator of the toroidal motor with turbines, figure Q represents the cold water tank, figure Y represents the gear tooth that drives the direct current electric generator from figure Z, figure AA represents the catchment water and steam from the outlet of the vertical toroidal motor with turbines figure E represents the large gear that ensures a constant rotation to all the turbines on the column and together with the gear of the generators force ensures the same speed to all vertical toroidal motors with turbines. In this invention we have 12 toroidal motors on the column and six toroidal motors on the horizontal.

Drawing No. 17: Represents the constructive assembly of part of the six columns and four rows of vertical toroidal motors with turbine in addition to drawing number 16, we have the water cooling system powered by freon and the figure of the fire cylinder area and figure V cylinder of the fire zone.

Drawing No. 18: Represents the top view of the six vertical toroidal motors with turbines, figure E represents the base plate and gears for synchronizing the speed between the vertical toroidal motors, figure B represents the intake adjustment system, figure DD represents the fire zone, figure BB represents the cooling system of the water and steam leaving the vertical toroidal engine with turbines figure AAA represents the cold water basin figure X represents the hydrophore, Figure A represents the intake of the toroidal engine, figure E represents the intake located in the area of the fire cylinder, figure CC represents the stator of the vertical toroidal turbine motor.

Drawing No. 19: Represents the constructive assembly for six columns and two rows of vertical toroidal motors with turbine.

Drawing No. 20: Represents the view in space of six columns and two rows of toroidal turbine motors, in addition on this drawing we have the coupling system Figure FF, between the gear wheel and the electric generator of direct current.

Drawing No. 21: Represents the top view in which we also have the FF intake system inside the fire cylinder.

Drawing No. 22: Represents the view of the vertical toroidal cylinder with turbines in front and side position, one for open intake at minimum and the other also for intake, open at maximum. Figure A represents the two intakes, figure C represents the stator of the vertical toroidal turbine motor, figure N represents the supply of cold water tank, figure Y represents the power gear, figure E represents the gear synchronization gear Rotation Take all toroidal motors vertically figure E 'represents the support or base-plate of the gears, figure B represents the intake adjustment system, figure Q represents the cold water tank figure A' represents the open intake at least inside the fire cylinder, figure N represents the cold water intake of the tank, figure A " represents the maximum open intake inside the fire cylinder.

Drawing No. 23: Represents the section by the vertical toroidal turbine engine. Figure KK represents the stator disc guide, figure GG represents the bearing balls which are 2/3 in the stator and one third in the turbine disc channel, figure HH represents the teeth on the turbine disc crown, figure MM represents the water and steam evacuation inside turbines, through the inside of the toroidal turbine engine the evacuation of water and steam takes place on the entire inner circumference of the toroidal turbine engine, figure LL represents the water outlet from the tank in the external water pressurization system that will enter above and below the pipes steam making a very high heat transfer so that the water entering the toroidal motor will have a temperature of 10 degrees Celsius, and the outlet of the toroidal motor together with the steam will have 70 degrees Celsius, figure Q represents the cold water tank, figure M represents the cooler that works with freon, figure KK represents the entry of cold water from the pipes into the water tank, figure L represents the water absorption system from the pressurized tank at the end entering the area of the steam tubes above and below the tubes, figure J Represents the water and steam guidance system for the evacuation through the inside of the turbine engine vertical toroidal with turbines that will wash the tank, and the water the steam will cool down a bit, figure R represents the steam inlet holes, figure H represents the turbine blade, figure C represents the stator, figure K represents the two turbine discs, figure KK represents the stator guide for the exhaust system, figure B represents the intake adjustment system.

Drawing No. 24: Detail of the water and steam supply system.

Drawing No. 25: Represents the top of the central rocket with the command center and cargo area. Figure one represents the central rocket, figure two represents the water basin that supplies the outer area of steam and also has the role of reducing vibrations from the propulsion system, for a comfortable life on board the ship, figure three represents the return of steam in the pressurization area by steam turbines, figure four represents the up and down steering cylinder with opposing turbines, figure five represents the toroidal drinking water tank, figure six represents the toroidal drinking water tank, figure seven represents the toroidal drinking water tank with system figure eight represents the thermal insulation system between the outer water cylinder 10 and the outer twelve and inner eleven steam cylinders, the new figure representing the ceiling support pillars, figure 14 represents the hydraulic system of the elevator figure 15 represents the hydraulic cylinder of the elevator, figure 16 represents a cosmonaut in the elevator being also an area of the shuttle control command, figure 17 represents the parabolic window.

Drawing No. 26: Represents the entire top of the central rocket with the command and control center and cargo area, we also have the elevator lifted off the shuttle with the cosmonaut.

Claims

Closed circuit space shuttle (in which no water, hvdroqen or oxygen is lost)(II) The Claims

1. Drawing No. 1: We have the vertical section through the rocket (The four rockets of the space shuttle are identical), section no. 1 in area A, of the steering control cylinder, view of the space shuttle from the outer rocket, the next view is the view of the space shuttle from the inner rocket. The positioning of the steering control cylinders in the outer missiles are positioned perpendicular to the radius of the inner missile, ensuring the rotation of the space shuttle. The inner rocket steering control cylinder is positioned within range, ensuring the maneuverability of the space shuttle, along with the second inner rocket steering control cylinder is mounted under the space shuttle control and cargo chamber, ensuring the maneuverability of the up and down direction, having a high maneuverability because the center of gravity of the rocket or the space shuttle is under the propulsion system.

2. Drawing No. 3: We have a vertical section through the rocket, section A1 from zone A, which represents the horizontal section A1 , having the following components: exterior wall, water area, walls that include thermal insulation, having the role of separating the water area and steam from the area vertical toroidal turbines, the four electric water pumps circulating in the area of vertical toroidal turbines engines in the area of cylinder 3 water and steam, the two electric water pumps circulating in the area of vertical toroidal turbines engines in the cylinder area 1 of water and steam, the horizontal toroidal system for cooling the steam from the steering control cylinder, the cooling is done by means of the internal heat transfer wings, the holes in the support plate for weight reduction, the horizontal toroidal hydro pump for circulating cold water up to the toroidal cold water tank located in the upper part of zone D, the structural role system supports you of the upper areas, steering control cylinder, turbine version.

3. Drawing No. 4: We have a horizontal section through the steering cylinder in zone A, with three variants of construction of the steering cylinder. The first construction is similar to the rocket propulsion system, the Micro double rocket system and micro turbines are on a much smaller scale and have only seven double rocket engines having two systems in opposition in the horizontal tube of the steering cylinder. The second construction version is equipped only with seven double rocket engines, and the third construction version with only two sets of turbines in opposition. In the atmosphere of the planet where the space shuttle is located, the double rocket system with opposing turbines must be used, and in outer space it is enough to use the set of two opposing turbines. They operate on short pulses depending on the direction of rotation or up or down direction, and operate one set of double missiles and turbines or the other set of double missiles and turbines on the opposite side. So that the steam from the horizontal toroidal system for cooling the steam is depressurized and pressurized by the two micro-turbines and forced to pass through the seven double missiles that work by burning oxygen and hydrogen, this water vapor generated will have a temperature and kinetic force quite sea that will pass through the cooling wings and will be directed by the steam directing cone to the cylinder walls, in the immediate vicinity behind the opposite system of double rocket and micro turbines we have six high pressure nozzles for cold water at 60 degrees between them which will spray cold water, through a slit a spray angle of 160 degrees covering almost the entire area of the cylinder circle, greatly reducing the steam temperature and kinetic energy so that the steam will pass at a much lower speed and a much lower temperature through the horizontal toroidal cooling system where it will be further cooled, reaching again the micro system propulsion with very low energy. This difference in kinetic and thermal energy from the moment it exits the propulsion power plant until it reaches the turbines again represents the energy with which the steering tube is pushed, respectively the rocket and of course the space shuttle. If the tubes of the outer missiles receive this impulse, the space shuttle will begin to rotate if we want to rotate it in the opposite direction. If we want to change the up or down direction, the steering tube for this purpose is mounted in the central rocket with one cylinder at the base of the rocket and the second cylinder is mounted below the control chamber and the cargo space. All space shuttle steering controls are executed by these tubes with opposing Micro propulsion systems.

4. Drawing No. 5: We have a horizontal section through the rocket, a Mini nuclear power plant in zone 8, we have the uranium nuclear reaction control system which is surrounded by heavy water which too much thermal energy of this reaction and will be given to distilled water which will turn into high temperature and pressure steam, steam will pass through 12 pipes inside the third cylinder of water and steam heating this area of cylinder 3. The remaining steam will continue and will reach the steam pressurizing turbines in the double rocket propulsion system.

5. Drawing No. 6: We have a horizontal section through the rocket in the C1 area, we have the first row of vertical toroidal motors with turbines at the bottom of the rocket having the inputs permanently open at maximum in rotating mechanical energy and is taken over by direct current electric generators powering the entire electrical system of the space shuttle. In the center in the fire cylinder we have represented the cone with drops directing the steam to the maximum permissible open to the vertical toroidal motors with turbines, to avoid the braking effect that could occur by touching the inner cover of the fire cylinder by the rest of steam. We have represented the pressure adjustment tubes in the area of the toroidal motors that maintain a constant pressure adjustment of 1.2 bar, this pressure adjustment is achieved by inserting the tube more or less in the fire zone directed downwards, so that the propulsion steam will it sucks steam from the area of the vertical toroidal engines with turbines through the 12 columns. We also have represented water cylinder 3 and steam thermal insulation between cylinder number three and cylinder area 2, steam water recovery area of vertical toroidal engines with turbines, cylinder 2 steam water recovery, thermal insulation between cylinder 2 and water cylinder 1 and steam and the outer wall of the rocket.

6. Drawing No. 7: We have the horizontal section through the rocket in zone C2, and the vertical toroidal motors with turbines to take the kinetic and thermal energy of the steam from the fire cylinder, this energy is transformed into mechanical rotational energy and is taken over by electric generators of direct current feeding the entire electrical system of the space shuttle, we have represented the fire cylinder, we have represented the cooling fins that take the thermal energy of steam and transmit it in cylinder number three of water and steam. Water supply to big fins is made from the zone of vertical toroidal motors which has turbines, and due to the washing of the inner walls of the large fins generates steam in the area of the third cylinder of water and steam, we also have represented the pressure adjustment pipes in 12 pieces in number maintaining a pressure of approximately 1.2 bar in the area of vertical toroidal motors with turbines. We also have represented the water and steam cylinder 3 with thermal insulation between cylinder 3 and the area of cylinder 2 intended for the recovery of steam water from the area of the vertical toroidal engines with turbine and the thermal insulation between cylinder 2 and cylinder 1 of water and steam and the outer walls of the rocket. In this board we also have represented the minimum open steam intake. At the top right of the drawing number seven we have represented the large wings and the small wings in vertical section.

7. Drawing No. 8: We have the horizontal section through the rocket in the F1 area, we have represented the section in all 19 double propulsion missiles, the small heat take-off fins, the three-cylinder steam thermal insulation between the three steam cylinder and the 2-cylinder, and the high horizontal toroidal tanks pressure for hydrogen on missiles on the outside and oxygen on missiles on the inside. We also have a section in the connection pipe between the high pressure toroidal tanks and the thermal insulation between cylinder 2 and cylinder 1 steam and the outer wall of the rocket.

8. Drawing No. 9: We have represented the vertical section through the propulsion system of the 19 double missiles, in which we can see the high pressure oxygen supply and the high pressure hydrogen supply, it can be seen that the steam pressure from the pressurizing turbine, creates steam pressure in the cylinders of the double rocket of the 19 engines washing the outer casing of the rocket engine inside and the rocket support fins that run on hydrogen and oxygen.

9. Drawing No. 10: We have represented the horizontal section by missile in section F2. We have represented the electrolysis system consisting of 10 concentric zones of hydrogen and alternating oxygen. The electrolysis system is permanently supplied with direct current generating oxygen and hydrogen by means of high pressure pumps. The high pressure tanks of the inner missiles are for oxygen, the high pressure tanks of the three outer missiles are for hydrogen. We also have represented the steam area pressurized by steam turbines, cylinder 3 water and steam, thermal insulation cylinder that separates cylinder 3 water and steam from cylinder 2, where the toroidal tank for electrolysis is located; we also have thermal insulation that separates the area of Electrolysis from cylinder 1 steam.

10. Drawing No. 11: We have represented vertical sections through the electrolysis system in zone F, and we have four drawings, drawing 1 we have represented turbine 2, driven by a direct current motor clockwise, turbine 1 driven by a direct current motor counterclockwise, turbine clamping and steam steering system, steam turbine outlet cone and a section of three twin-rocket engines with the feed system, power supply from the oxygen turbine driven by an electric motor from the turbine of hydrogen by an electric motor, both with direct current, we have represented a cylinder one steam thermal insulation that prepares the electrolysis area of cylinder 1 , steam and the outer wall, also represented is the toroidal tank for capturing hydrogen from electrolysis, and below we have the tank toroidal for capturing oxygen from electrolysis and below it we have the toroidal electrolysis system with negative bus bar, they negative electrodes and positive electrodes. In drawing number two, we have the same representation as in drawing one, in addition we have the oxygen supply tubes from the electrolysis to the toroidal capture tank. In drawing 3 we have the same representation as in drawing 1 , in addition we have a positive bus bar representation, in drawing four we have represented the same as in drawing number two in addition we have the hydrogen supply tubes of the capture tank located above the Electrolysis.

11. Drawing No. 12: We have represented half of the vertical toroidal turbine engine. Figure A, Represents the intake together with the intake adjustment system B, from minimum to maximum, Figure C represents the stator of the vertical toroidal turbine engine, together with the figure E of the gears, with the bars D, of the resistance of the state, Fig F represents bearings on which are mounted 2/3 in stator one third slide on the channel of the two turbines, figure G represents the cover of the turbine blades, figure H represents the blade system of the turbine, figure I represents the cylinder detachment of the blades with the steam passage holes, figure J represents the system of directing the steam towards the inside of the torus, figure K represents the cover of the turbine blades, figure L represents the water supply system from the tank ie from inside the toroidal engine to the outside, figure M represents the cooling system of the water entering the tank, figure Q represents the water tank which is fed from the outside through the hole in figure N and given to the toroidal motor through the holes of the re water tank figure N.

12. Drawing No. 13: We have an exploded diagram of half of a vertical toroidal motor with turbines in addition to Drawing number 12, we have figure Q of the clamping system for the intake adjustment system and figure T represents the Freon supply port of the cooling system M.

13. Drawing No. 14: We have represented in great detail the turbine system, together with the disc with holes and pipes and the water and steam guidance system towards the inside of the vertical toroidal turbine engine. Figure H represents the turbine blades, figure G represents the steam inlet area, figure R represents the steam steering tubes, figure J represents the water and steam guidance system inside the vertical toroidal turbine engine, figure G represents the outer cover of the turbine, figure H represents the turbine blades, figure I represents the disc where the turbine blades are located, figure T represents the inlet holes in the pipe figure R, and figure J represents the water and steam guidance system from inside the vertical toroidal turbine engine.

14. Drawing No. 15: We have in detail the system for collecting cold water from the tank and pressurized the outside entering through the holes of figure S. Above and below the steam pipes in figure R, Figure one represents the teeth of the crown of the inner cover of the turbines, figure L represents the slats of the water collection system from the tank and pressurized at the end, figure a represents the cold water tank figure P represents the holes in the supply tank of the L water collection system and pressurized outside. Figure V represents the freon supply port of the cooling system in figure M, figure N represents the supply port of the cold water tank.

15. Drawing No. 16: Represents the constructive assembly of six columns and four rows of vertical toroidal motors with turbine, figure X represents the hydro-pump, Figure W represents the cold water supply pipe from the hydro-pump, figure V represents the third cylinder of the fire zone, figure A represents the intake of the vertical toroidal motor with turbines, figure C represents the stator of the toroidal motor with turbines, figure Q represents the cold water tank, figure Y represents the gear tooth that drives the direct current electric generator from figure Z, figure AA represents the catchment water and steam from the outlet of the vertical toroidal motor with turbines figure E represents the large gear that ensures a constant rotation to all the turbines on the column and together with the gear of the generators force ensures the same speed to all vertical toroidal motors with turbines. In this invention we have 12 toroidal motors on the column and six toroidal motors on the horizontal.

16. Drawing No. 18: Represents the top view of the six vertical toroidal motors with turbines, figure E represents the base plate and gears for synchronizing the speed between the vertical toroidal motors, figure B represents the intake adjustment system, figure DD represents the fire zone, figure BB represents the cooling system of the water and steam leaving the vertical toroidal engine with turbines figure AAA represents the cold water basin figure X represents the hydrophore, Figure A represents the intake of the toroidal engine, figure E represents the intake located in the area of the fire cylinder, figure CC represents the stator of the vertical toroidal turbine motor.

17. Drawing No. 22: Represents the view of the vertical toroidal cylinder with turbines in front and side position, one for open intake at minimum and the other also for intake, open at maximum. Figure A represents the two intakes, figure C represents the stator of the vertical toroidal turbine motor, figure N represents the supply of cold water tank, figure Y represents the power gear, figure E represents the gear synchronization gear Rotation Take all toroidal motors vertically figure E 'represents the support or base-plate of the gears, figure B represents the intake adjustment system, figure Q represents the cold water tank figure A' represents the open intake at least inside the fire cylinder, figure N represents the cold water intake of the tank, figure A " represents the maximum open intake inside the fire cylinder.

18. Drawing No. 23: Represents the section by the vertical toroidal turbine engine. Figure KK represents the stator disc guide, figure GG represents the bearing balls which are 2/3 in the stator and one third in the turbine disc channel, figure HH represents the teeth on the turbine disc crown, figure MM represents the water and steam evacuation inside turbines, through the inside of the toroidal turbine engine the evacuation of water and steam takes place on the entire inner circumference of the toroidal turbine engine, figure LL represents the water outlet from the tank in the external water pressurization system that will enter above and below the pipes steam making a very high heat transfer so that the water entering the toroidal motor will have a temperature of 10 degrees Celsius, and the outlet of the toroidal motor together with the steam will have 70 degrees Celsius, figure Q represents the cold water tank, figure M represents the cooler that works with freon, figure KK represents the entry of cold water from the pipes into the water tank, figure L represents the water absorption system from the pressurized tank at the end entering the area of the steam tubes above and below the tubes, figure J Represents the water and steam guidance system for the evacuation through the inside of the turbine engine vertical toroidal with turbines that will wash the tank, and the water the steam will cool down a bit, figure R represents the steam inlet holes, figure H represents the turbine blade, figure C represents the stator, figure K represents the two turbine discs, figure KK represents the stator guide for the exhaust system, figure B represents the intake adjustment system.

19. Drawing No. 25: Represents the top of the central missile with the command center and cargo area. Figure one represents the central rocket, figure two represents the water basin that supplies the outer area of steam and also has the role of reducing vibrations from the propulsion system, for a comfortable life on board the ship, figure three represents the return of steam in the pressurization area by steam turbines, figure four represents the up and down steering cylinder with opposing turbines, figure five represents the toroidal drinking water tank, figure six represents the toroidal drinking water tank, figure seven represents the toroidal drinking water tank with system figure eight represents the thermal insulation system between the outer water cylinder 10 and the outer twelve and inner eleven steam cylinders, the new figure representing the ceiling support pillars, figure 14 represents the hydraulic system of the elevator figure 15 represents the hydraulic cylinder of the elevator, figure 16 represents a cosmonaut in the elevator being also an area of the shuttle control command, figure 17 represents the parabolic window.

20. "Interplanetary transport”: If we have to move to Mars. After leaving the Earth's outer space, the shuttle will head for the sun for a few weeks, so the space shuttle will rotate around the imaginary axis directed directly at the center of the sun, so that the space shuttle's axis will be almost perpendicular to the sun's rays the possibility that a larger surface of the space shuttle will be exposed to sunlight and also the space shuttle will have a rotation around its axis, the rotation will be about three rotations per minute so that the shuttle will heat evenly over the entire surface. This heating of the shuttle leads to the heating of the water and to the production of steam from the area of the outer cylinder inside the rocket and the outer area of the support wings of the rockets. This steam will be depressurized from the outer steam and water area of cylinder 3 pressurized by the steam turbines and forced to pass through the Cylinder of each Double Rocket Engine. The passage of steam through these cylinders will be further accelerated because around the cylinders are fins that have inside them electric heating elements of steam heating, these electrical resistances are located in the support fins and the fins around the support cylinder of the rocket engine. These fins are constructed in such a way that the steam resulting from the propulsion has a minimum friction with these fins. The electric steam heaters in the rocket-propelled fins that run on oxygen and hydrogen will be powered by electricity all the time, but especially when the entire propulsion system will run on steam only. The electric steam heating elements mounted in the fins which are mounted all around the entire length of the propulsion system cylinder and can be supplied throughout the operation, further increasing the temperature of the superheated pressurized steam generating an even higher kinetic and thermal energy superheated pressurized steam propulsion, it should be noted that the propulsion system will never be stopped (only in case of failure) can operate from 5% to 100% of the rated power of the propulsion system, only in special cases of strict necessity in the short term, the rated power of the propulsion system can increase up to 150% but in a very short time. After a substantial increase in speed, and the full loading of the horizontal toroidal tanks of oxygen and hydrogen, the space shuttle will move to Mars, the space shuttle will begin to rotate around the axis of travel to the North of Mars and due to the continuous increase in speed. The radius of rotation of the space shuttle around the imaginary axis of direction, the radius will increase to tens of thousands of kilometers. If the space shuttle rotates perpendicular to the direction of travel, the proximity to Mars will be the same as when it began to move in the direction of Mars, and if the space shuttle rotates 90 degrees in the direction of Mars, it will result results in a constant speed approaching Mars (even if we have a continuous increase in speed) in the direction of travel and will be 120 degrees in the direction of travel, and the speed approaching Mars will increase again if the rotation in the direction of the axis to the north of Mars will be behind it, ie 60 degrees from the direction of travel we have a decrease in the speed of approaching Mars, it will be like a screw when the speed remains constant compared to approaching the planet Mars, this imaginary screw will have a step of the imaginary screw thread. When we want to increase the speed of the approach to the planet Mars we increase the step of the imaginary screw, and if we want to decrease the speed of the movement towards the planet we decrease the step of the imaginary screw. This condition is also necessary to expose the space shuttle perpendicular to the sun's rays if the direction of travel to Mars is perpendicular to the sun's rays, the space shuttle will no longer need to rotate in the imaginary axis, and its approach speed will be higher, respectively the deceleration speed will be higher. The space shuttle will have an increase in speed between 0.1G and 1G (gravity on the ground) during this trip, this speed depends on the energy it captures from the sun's rays, so the space shuttle must move perpendicular to the sun's rays and rotate all the time around its axis with a homogeneous heating, with a greater exposure of the space shuttle to solar radiation, they will heat the space shuttle more and at the same time the water and steam that will be used for propulsion space shuttles at the same time with the continuous increase of speed and the production of electricity that feeds the entire space shuttle and especially of the electrolysis tanks, loading the toroidal tanks with Hydrogen and Pressurized Oxygen at very high pressure. This energy of hydrogen and oxygen will be used almost completely until the space shuttle reaches the very rarefied atmosphere of Mars at the top (Take the pole of Mars) but will begin to recharge from the moment it touches the planet's atmosphere. Due to the high speed of the space shuttle of over 200,000 Km / h, the speed reached during the trip, but which must start to slow down at the space shuttle almost halfway to reach the atmosphere below 50,000 Km / h, usually the devices NASA's spacecraft reaches the atmosphere of Mars at a speed of approximately 25,000 km / h, and does not recover any of this frictional energy with the atmosphere, but the space shuttle helped by the rocket effect given by the double rocket engine due to the energy of steam, steam generated by rubbing with the atmosphere of the planet Mars, the space shuttle is directed towards the center of the planet a little after moving to reduce the speed of movement so that it can remain in the very rarefied atmosphere of the planet Mars not to be rejected in outer space. The steam is formed due to the energy obtained by the friction of the space shuttle with the atmosphere of the planet Mars. As the distance begins to shrink further from Mars, the space shuttle moves in a direction perpendicular to the radius of the planet, and the braking will be done with a force of 1 G maximum 2G, and will begin to navigate around Mars , in the super-thin atmospheric space helped by the rocket effect of the propellant steam, generates a better control over the Navigation of the Space Shuttle and the distance from the planet Mars will decrease very very slowly, making 30 ... 50 rotations around the planet Mars, The deceleration force (braking) of space shuttles will never exceed 2 G (twice the gravitational force of the earth, for a comfortable life of astronauts), during which the friction with the atmosphere makes the space shuttle heats up and of course the heating of the water generates steam from the outer cylindrical tank 1 inside the rocket feeding the propulsion system and of course the production of electricity, which will be used in s especially take the electrolysis system by filling the horizontal toroidal tanks with hydrogen and oxygen. Arriving on Mars with the horizontal toroidal tanks of hydrogen and oxygen almost full.

21. “Interstellar transport”: After exiting into outer space, the space shuttle will head for the sun past Venus and orbit the Sun (between Venus and Mercury) for several months, perpendicular to the sun's rays for much more energy. At the same time, the space shuttle will rotate around its axis approximately one rotation per minute, even every two minutes, for a homogeneous heating of the space shuttle, during which time the speed of the space shuttle will increase. Due to this, the speed of the ship will always increase by about 1G. And due to the construction of the space shuttle surrounded by water and steam, cosmonauts will be very much protected from solar radiation so the speed will increase greatly, more than 10 percent of the speed of light, to NOT go out of orbit at the sun at this very high speed , the axis of the space shuttle will be directed a little to the sun, we stop the shuttle for a short time the shuttle will be projected tangentially in the direction of travel. It should be noted that this direction must be on the axis of movement of the sun + - 70 degrees so that the shuttle does not enter the solar system and will be directed to the nearest solar system "proxima" which is located at a distance of 4 years light so that in 40 years we can reach the nearest solar system, compared to current technology the time to the nearest solar system is several thousand years. If we consider "quantum physics" according to which in the space between planets between solar or galactic systems "is not empty and without energy" and that we have an energy fluctuation and there are several tens of hydrogen atoms per cubic meter, so using this information, the space shuttle will move perpendicular to the forward direction, rotating around the axis of movement, exposing to the maximum the surface of the space shuttle. By heating the space shuttle outside enough to accumulate an energy of growth at a speed of over 0.1G for a life as comfortable as possible for astronauts during this time, it should be mentioned that this speed and a piece of paint is catastrophic for the space shuttle. Arriving in the new solar system of course at a slightly lower speed due to the bombardment of space shuttles by hydrogen atoms (a few atoms per cubic meter), and as this speed is still too high to go to the desired planet in the new solar system, we must we orbit the new sun for several months so that we can use the energy accumulated by it so that we can brake considerably. Reaching a speed below 100,000 Km / h, and only then to go to the desired planet. Too bad our life is so short, even if we had a shuttle that could reach half the speed of lightning, it would still take us 200,000 years to cross our galaxy (the Milky Way) from side to side, or if we didn't If we were to move perpendicular to the Milky Way, it would still take several thousand years for us to be able to photograph our galaxy from one end to the other in fullness of its beauty.

22. “Transport around Earth”: If the space shuttle moves from Bucharest to Tokyo, the energy consumed to reach space is recovered by the Sun and especially by the friction of the space shuttle with the atmosphere, which will heat the outer surface of the space shuttle, this makes water to be overheated generating steam for propellants, for better maneuverability and especially for driving vertical toroidal motors with turbines that take the kinetic thermal energy of the steam from the fire cylinder, driving the electric generators of direct current (we do not need electric batteries space shuttle) so that much of this electricity will be used to power the electrolysis plant, generating oxygen and hydrogen so that the high pressure toroidal tanks will be refilled with hydrogen and oxygen, so after landing the spacecraft is ready to takeoff. The maneuverability of advancing the Space Shuttle is done with the help of tubes with two rocket engine systems in opposition, these tubes are placed above the landing system in the three outer rockets perpendicular to the radius of the central rocket resulting in the rotational movement of the space shuttle. The lower part of the steering wheel is made by the two cylinders with opposing rocket engines, located in the central rocket, one tube above the landing system and the other tube below the control system and the cargo area of the central rocket.