SI26013A - Spacecraft powered by electromagnetic waves with primary and secondary tunnel for accelerating in the vacuum and generating electricity to propel the craft - Google Patents

Abstract

The subject of the invention is a spacecraft on electromagnetic waves with primary and secondary tunnels for acceleration in airless space and obtaining electricity to power the vessel. Its advantages are that it does not pollute the environment, it is suitable for long flights, it is almost inaudible, and it obtains electricity from its own electromagnetic waves. It takes off less energy on takeoff than existing spacecraft. The crew is protected from cosmic radiation. The crew member (A) and (B) rotate in opposite directions in space, allowing gravity to rotate in the living space of element (A), creating a centrifugal force that lands personnel on the space. The vessel needs smaller hydrogen-powered power units (BI11) to charge the batteries (BII4) if all else fails. The vessel can also be fitted with wings of any shape, on which additional solar cells (BI10) are installed. The vessel is modularly detachable, which enables easier maintenance.

Description

SPACE ON ELECTROMAGNETIC WAVES WITH PRIMARY AND SECONDARY TUNNELS FOR ACCELERATION IN AIRLESS SPACE AND GENERATION OF ELECTRICITY FOR DRIVING A VESSEL

The subject of the invention is an electrically powered spacecraft, more specifically, an electromagnetic spacecraft with a primary and secondary tunnel for accelerating in airless space and obtaining electricity to power a spacecraft that can move in the atmosphere or airless space. It is a vessel that has the ability to accelerate, turn and brake in an airless space or atmosphere.

The technical problems solved by the invention are: how to enable the possibility of acceleration in airless space, how to achieve lower fuel consumption on takeoff, how to turn and brake the aircraft in airless space, how to allow the crew artificial gravity, how to protect the crew from cosmic radiation and how to reduce the speed of the vessel before it enters the atmosphere and when landing in the atmosphere without the use of an additional speed inhibitor such as a parachute. It also solves the problem of constant acceleration in airless space.

BACKGROUND OF THE INVENTION: Spacecraft mostly use chemical propulsion (oxygen, hydrogen and solid fuels, methane ...) to take off from Earth through the atmosphere to overcome Earth's gravity. Ionic engines (which use a gas such as xenon) to travel across interplanetary space. Both engines have a problem of braking before entering the atmosphere of the target planet. Contrary to known solutions, the present invention allows the vessel to enter the atmosphere at a reduced speed and does not need a parachute when landing. A vertical landing is planned. The vessel does not pollute the environment and emits minimal noise during the voyage.

Some additional operating principles used by the vessel according to the invention are already described in patents SI9300414 (W09504900A2), SI24404 (WO2014209240A4), SI24409 (WO2014204412), SI24931 (W02016130093A1) and SI25331 (WO201811). sliding power transmission, braking and sealing with orings, and fastening with blockers, so we will not describe them again here.

The invention is described by means of an embodiment and in the drawings showing:

Figure 1: element A - living space in the vessel in which magnets and bearings are spirally mounted inside

Figure 2: Element B with spirally mounted magnets, bearings and windings

Figure 3: Cross section of element B with tunnel, shaft, funnel inlet and funnel outlet

Figure 4: Fans, rod supports and light source on the shaft, blockers that are part of element B are also shown

Figure 5: View of the turbulators installed at the exit of the vessel: showing how they are attached to the lower axle and showing the BII19 telescopic antenna

Figure 6: Illustration of the installation of magnets on turbulators and grooves or slats at the funnel inlet

Figure 7: Installation of fans and drill accelerator

Figure 8: floor plan of rod-shaped turbulators and hydraulic blockers in the lower part of the vessel at the funnel exit

Figure 9: View of the side accelerator and rudder of vessel E

Figure 10: Floor plan of the entire vessel with all side accelerators and rudders of vessel E

Figure 11: View of the blockers in the upper part of the vessel for the BI cylinder and the BI3 telescopic cylinder with BI5 and BI7 orings

Figure 12: view of the BI3 cylinder in the lowered position in the lower part of the vessel with solar cells BI 10 and the vacuum assembly BI9 and the telescopic antenna BI119 in the extended position

Figure 13: View of the whole vessel with all elements A, B, Bil, C, D E and BII19

Figure 14: View of the entire vessel with cylinder BI3 in the extended position when forming a secondary tunnel with antenna BII19 in the extended position

The specific reference marks in the drawings represent the following components of the vessel according to the invention:

Element A: Vessel crew accommodation rotates around element B, creating artificial gravity for crew

Element B: as a spacecraft stator and accelerator of photons and electrons against magnetic turbochargers

Element C: central accelerator with fans C6 attached to the shaft of element B, rod beams Cl, light source C2,

Element D: Turbolators in the lower part of the vessel at the funnel exit

Element E: Side Accelerator and Vessel Guide - This element helps to stabilize the vessel on take-off and turn, and when accelerating in airless space, composed similarly to element B with an acceleration tunnel and funnel-shaped entry and exit

Al and BI: bearings at the funnel entrance

A2 and B2: magnets spirally mounted along the funnel-shaped entrance and opposite each other

A3 and B3: bearings before entering the tunnel

A4 and B4: bearings over the entire circumference

A5 and B5: magnets routed around the entire circumference to allow rotation

A6 and B6: bearings in front of magnets for generating electricity

A7 and B7: magnets A7 in the middle of the vessel and winding B7, which allows the rotation of the elements to generate electricity.

A8 and B8: bearings across the entire circumference that allow rotation

A9 and B9: magnets that spiral over the entire circumference and allow constant rotation

A10 and B10: bearings around the entire circumference before the funnel exit

Ali and Bil: bearings at the beginning of the funnel exit

A12 and B12: the magnets are helically routed across the funnel outlet

A13 and B13: bearings before funnel outlet

Bill: outer cylinder

ΒΙ2: spirals around the circumference of the outer cylinder Bil

BI3: inner cylinder between outer cylinder Bil and element A

BI4: spiral running through the inner cylinder BI3

BI5: upper orings on element B

BI6: lower orings on element B

BI7: orings on inner cylinder BI3

BI9: vacuum circuit

BI10: solar cells inside the BI3 cylinder, also installed inside the Bil cylinder and in the E23 cylinder, from inside and outside this cylinder

Bill: an electric generator on hydrogen

BI12: ring on the inside of the cylinder BI3, which locks the inner cylinder BI3 in the lower part of the element B

Bill: space for batteries, electronics, windings, electrical generators, telescopic antenna, vacuum assembly and electrodes

BII2: capacitor

BII3: diode

BII4: batteries

BII5: hollow shaft running through the entire tunnel, the tubular beams BI 16 being made aerodynamically

BII6: brackets for the entire BI 15 and BI 17 shafts, cables and electrodes can be routed through them

BII7: lower part of the axis to which the magnetic turbulators are attached and in which the telescopic antenna is installed

BII8: telescopic legs

BII9: element carrier E

BII10: electrodes routed across the entire shaft to the Billi protective cap

Billi: a pointed protective cap that protects the electrodes on element B

BII12: source of light that excites electrons

BII13: winding

BII15: lamellas or grooves, help to rotate currents in element B

BII16: funnel-shaped outlet

BII17: grooves on Billy's pointed caps

BII18: funnel entrance

BII19: telescopic antenna

Cl: fluffy stabilizers that stabilize the hollow shaft BI 15 in the center of element B

C2: light source on the hollow axis opposite the light source BI112

C3: hydraulic bar stabilizer locks mounted on the hollow shaft and element B

C4: Electromagnets at the end of the blades on the fans

C5: rotor to which C6 fans are mounted

C6: fans

C7: magnetic bearings (can also be different types of bearings)

C8: winding that allows rotation with C9 magnets

C9: rotor magnets

CIO: power cables with E8 connectors and blockers as shown in Figure 9

CII: full fan bracket mounted on hollow shaft BII5 ^{mounted on VOtl} ° ^{shaft Bl15 and} P ° ^ve ^ ns with rod brackets Cl and hydraulic blockers C3 stabilize shaft BII5 in center

Dl: funnel-shaped entry on turbulators

D2: hollow shaft, fan holder D6 and drill accelerator D7

D3. rod beams attached to the B element in the lower part on the BII7 axis

D4: rings holding rod-shaped turbulators D3

D5: rings mounted on the lower axis BII7 and holding the turbulators

D6: fans mounted on the D2 axis

D7: Drill accelerators that rotate currents

DS: Electromagnets routed around the entire circumference of the turbulator, which enable acceleration in the airless space of electrons and photons, are spirally routed

D9: Slightly arched grooves to help rotate currents

D10: Power cables with E8 connectors and hydraulic locks, as shown in Figure 9

El: side accelerator and guide mounted on the outer cylinder Bil

Eli: side accelerator and guide mounted on the outer cylinder Bil

Elll: side accelerator and guide mounted on the outer cylinder Bil

EIV: side accelerator and guide mounted on the outer cylinder Bil

El. ring, holder of side accelerators and guides El, Eli, Elll, EIV

E2: hydraulic bar brackets E5

E3: upper shaft at funnel inlet BII18

E4: lower axle on extended outlet

Ε5: fluffy stabilizers

E6: ring in the center of the shaft, fixed with rod brackets

E7: Ring in the center of the lower axle and turbulator holder

E8: hydraulic locks in shaft and element

E9: pipes spirally from E10 turbulators to extended exhaust and · - ...

E10: entry of photon and electron currents into turbulators

Eli: Electromagnets in which E9 spiral tubes are installed

E12: electrodes routed inside the E3 shaft

E13: light source

E14: winding

E15: fan

E16: fan blades

E17: Electromagnets at blade ends

E18: Protective cap of honeycomb shape, which protects the electrodes on the element E

E19: grooves on the cone-shaped protective stroke

E20: grooves at the funnel entrance

E21: exit from turbochargers

E22: Telescopic antenna pushed into the lower part of the E4 shaft

E23: telescopic cylinder

E24: Spiral through half of cylinder E23

E25: blockers

E26: Cylinder lock holes E23

E27: fans in turbochargers

The spacecraft is powered by an electric drive, which uses electric light and magnets for its operation. It consists of the following basic elements: living space A which is built from the outside into an element with acceleration tunnel B and Bil, in which there is a vacuum and lined with material ^{Stlka 2 Central} Accelerator with photons and electrons C, containing fans Ce 'attacked on the axis of element B, rod beams Cl, light source C2, in which partial ^{magnetic turbuses are performed |} 3torjem D, located in the lower part of the vessel while on each! the side accelerators and rudders of the vessel E attached to it by which ^P. k ° ° ^braČa ' ^{n P} ° ^{SPEŠUJE V bre22raČnem brost} ° - Povilo can be built-in here ^ of any shape and is modularly detachable.

Before the spacecraft takes off, it stands upright, and all other telescopic elements except the BII3 legs are in the Folded state, ie: outer cylinder Bil, inner cylinder BI3 And also telescopic antenna BII19, which is telescopically pushed into the lower part of the BII7 axis. When the process of taking off from the ground in the atmosphere begins, all four side accelerators and rudders El, EH, Elll and EIV, mounted on the outer cylinder Bil on BII9 carriers, which can otherwise rotate, face the ground. The side accelerators and routers El, Eli, Elll and EIV are also in a folded state. The E22 telescopic antenna is pushed into the lower part of the E4 shaft. The E23 cylinder is lined on the outside and inside with BI10 solar cells. Between the internal and external solar cells BI10, there is a spiral E24 in between, through which gas or liquid flows. The E24 coil cools or heats the E23 cylinder if necessary. In the lower element E, all four E27 fans in the E10 turbochargers are switched on, the Eli electromagnets are switched off. Then turn on the fan E15 in the primary tunnel of element E. Other elements: E12 electrodes, E13 light source, Eli electromagnets, E17 blade end electromagnets and E14 winding are switched off. When the E27 fans in the D turbochargers are in operation, they stabilize the spacecraft and help it overcome gravity. Then in the lower primary tunnel of element B turn on fans D6 in turbochargers D and finally fans C6 in the upper part of the primary tunnel of element B. Then in the lower primary tunnel of element B all other elements: electrodes BII10, windings BII13, electromagnets D8, electromagnets at the ends blades C4, light source BII12 and light source C2 on the BII5 axis when the spacecraft travels in the atmosphere off.

When the spacecraft takes off and overcomes the planet’s gravity, we get into airless space. There, the processes of acceleration to electromagnetic waves begin. Therefore, we start to turn on the individual elements in the following order: first the inner cylinder BI3 slides along the vessel between the inner cylinder Bil and stops at a certain point, locked with a ring ΒΙ12, which is at the top of the cylinder BI3. The BII19 telescopic antenna, which is pushed into the lower part of the BII7 shaft, is also telescopically stretched hydraulically. Then the primary processes in the element B tunnel begin - the acceleration of the spacecraft in airless space. The BII10 electrodes, which protrude slightly from the BI 15 shaft, and the BII5 shaft also protrude slightly (protrude) in front of the vessel and the funnel inlet BII18. The BII10 electrodes spray electrons in front of the funnel-shaped BII18 inlet, which the vessel pulls inward during the flight. The BII15 lamellas help to rotate the currents and the electrons enter the primary tunnel of the B element during inward traction and pass through the light field created by the BII12 and C2 light sources. The lights radiate opposite. In this light field, photons excite electrons (see Figure 13). C6 fans now run at a lower speed. There are also C4 electromagnets at the ends of the E17 blades, and when the winding B13 is under current, an electromagnetic field is created where the electromagnetic currents are partially amplified. During further traction, electromagnetic currents from the primary tunnel of element B enter the turbulators D, where the electromagnetic currents in electromagnets D8 and drill accelerators D7 are amplified and further rotated. The amplified electromagnetic currents pass into the telescopically extended secondary tunnel of the inner cylinder BI3. Amplified electromagnetic currents push the spacecraft on electromagnetic waves emitted by the BI 119 telescopic antenna and received by the BI3 cylinder. Thus, in this BI3 tunnel, where BI10 solar cells are attached, two processes take place: the process of pushing the spacecraft and obtaining electricity for the needs of the spacecraft, while charging BII4 batteries in a similar way as in solar power plants.

On the inside of the Bil cylinder are BI10 solar cells, which come into play when the Bil cylinder is further lowered along the BI3 cylinder, thus further extending the BI3 secondary tunnel and gaining additional electricity with the BI10 internal solar cells.

In the jacket of the cylinder Bil, a spiral BI2 was passed, through which gas or liquid flows and protects the crew in the living space of element A from cosmic radiation. The BI4 spiral in the BI3 cylinder jacket has the same function.

On the outside of the BI3 cylinder, BI10 solar cells are mounted, as well as on the E23 telescopic cylinder, which can be used to generate electricity from the sun or stars. If the spacecraft is far away from the stars, we generate electricity only in the secondary tunnels formed by cylinders BI3, Bil, and in the four side accelerators El, EH, Elll and EIV with cylinders E23 when in the extended (stretched) position and by means of telescopic antennas BII19 and E22 with mixed amplified electromagnetic currents and waves. Thus, the processes of pushing the spacecraft and obtaining electricity and charging BII4 batteries are performed.

Hydrogen is obtained from water by electrolysis for the needs of auxiliary electric generators on hydrogen in Bosnia and Herzegovina. The spacecraft is generating electricity with BI10 solar cells and Bill's hydrogen auxiliary power generators in the event of a failure of the BI 10 solar cell system and other elements crucial to generating electricity.

Landing of the vessel: before the spacecraft reaches its destination, the braking processes begin. At that time, the two side accelerators and the routers El and Eli (in Figure 10) rotate 180 degrees. The other two Elll and EIV, however, remain in the same position. Routers push in pairs in opposite directions and turn the spacecraft. In the primary tunnel of element B and the secondary tunnel of element B formed by cylinder BI3 in the extended position, the thrust processes are stopped so that fans C6, magnets C4, electrodes C4, electrodes BII10, winding BII13 and turbulators D with fans D6 stop and are in phase rest. When the entire spacecraft is rotated 180 degrees, the El and Eli routers return to their original position, so that all four El (EIV) routers are facing in the same direction, ie in the direction of braking. In the primary tunnel of element B and in the secondary tunnel of element B, which is formed by the cylinder BI3 in the extended position, all the previously listed elements start working again and the braking process begins. When the spacecraft reaches its destination (Earth, Moon, another planet ...), it orbits the planet in airless space long enough to reach the ideal speed, and when this is reached, the telescopic cylinder E23, telescopic antenna E22, outer cylinder Bill and telescopic antenna Bill 19 return to folding condition. Electrodes ΒΙΙ10, winding BII13, electromagnets D8 and electromagnets Eli are stopped. The light sources E13 and C2 are also switched off. Only all C6, D6, E27 and E15 fans still work. The speed of these fans is regulated by electronics. When the vessel reaches the appropriate speed, it enters the atmosphere and lands vertically at the desired location without the need for a parachute, but brakes and lands in a controlled manner by regulating the speed of all C6, D6, E27 and E15 fans.

In the middle of the outer cylinder Bilje, a spiral BI2 runs through the entire circumference. Gas or liquid circulates through it. Thus, the external cylinder Bil with spiral BI2 protects against cosmic radiation element A, where the cabins with crew. The inner cylinder BI3 and the orings BI5 and BI6 on the element B and the orings BI7 on the cylinder BI3 seal the space between the element B and the cylinder Bil. There is a vacuum in this space, which is achieved with the BI9 vacuum assembly. The vacuum allows us to rotate element A more easily and reduces the noise of the vessel in the atmosphere. Air enters this space only when the crew wants to get out of the spacecraft.

The advantages of the spacecraft are: the spacecraft will not pollute the environment, will be suitable for long flights, will be almost inaudible, will generate electricity from its own electromagnetic waves, will not need a nuclear reactor or ion engine, which can only have a limited amount of fuel. It will be powered by its own electromagnetic waves, regardless of the presence of the sun and stars. It will use less energy on takeoff than today's spacecraft. The crew will be protected from cosmic radiation. Elements A and B rotate in opposite directions in space (airless space), which allows gravity due to constant rotation in the living space of element A, creating a centrifugal force that lands personnel in space. The vessel will need smaller Bill hydrogen generators, which will charge BII4 batteries if all else fails. Bill's power generators will only be turned on at takeoff. When the vessel overcomes the planet’s gravity, these aggregates shut down. The vessel can also be fitted with wings of any shape, on which additional BI10 solar cells are installed. The vessel is modularly detachable, which enables easier maintenance.

Claims (10)

1. Electromagnetic wave spacecraft with primary and secondary tunnels for airless acceleration and power generation to power the vessel, characterized in that it is powered by an electric propulsion system that uses electricity, light and magnets for its operation and consists of the following basic elements: living space (A), which is built from the outside into the element with the acceleration tunnel (B and Bil), in which there is a vacuum and is lined with light-reflecting material, elements (A) and (B) are in they rotate in opposite directions in the airless space, which allows gravity due to constant rotation in the living space of element (A), element (B) further contacts the central accelerator with photons and electrons (C), which contains fans (C6) attached to the element axis. (B), rod beams (Cl), light source (C2), in which partial processes of acceleration of currents against magnetic turbulators (D) located in the lower part of the vessel are carried out, while side accelerators and rudder guides (E) attached to each side, with which the vessel can turn and accelerate in airless space, and part of the element (E) is also a cylinder (E23), which is lined on the outside and inside with solar cells BI10), between which a spiral (E24) is passed, through which gas or liquid flows and with it, if necessary, cools or heats the cylinder (E23), and the vessel can also be fitted with wings of any shape and is modularly detachable. The spacecraft according to claim 1, characterized in that it stands vertically before its take-off, and all other telescopic elements, except the legs (BII8), are in the folded state, ie: outer cylinder (Bil), inner cylinder (BI3) and a telescopic antenna (BII19) that is telescopically pushed into the lower part of the shaft (BII7). Spacecraft according to Claims 1 and 2, characterized in that at the start of take-off from the ground in the atmosphere, all four side accelerators and guides (El, Eli, Elll and EIV) are mounted on the outer cylinder (Bil) on the supports (BII9 ), facing the ground, side accelerators and guides (El, Eli, Elll and EIV) are folded, telescopic antenna (E22) is pushed into the lower part of the shaft (E4), in the lower element (E) turn on all four fans E27) in turbochargers (E10), electromagnets (Eli) are turned off, then turn on in the primary tunnel element (E) fan (E15), other elements: electrodes (E12), light source (E13), electromagnets (Eli), electromagnets on the blade ends (E17) and the winding (E14) are switched off. Spacecraft according to claims 1 to 3, characterized in that when the fans (E27) in the turbochargers (D) are in operation, stabilize the spacecraft and help it overcome gravity, then turn on the fans in the lower primary tunnel of element (B) (D6) in the turbochargers (D) and finally the fans (C6) in the upper part of the primary tunnel of the element (B). A spacecraft according to claims 1 to 4, characterized in that s that when it takes off and overcomes the planet's gravity, the processes of acceleration to electromagnetic waves begin, so we begin to turn on the individual elements in the following order: first the inner cylinder (BI3) slides along the vessel between the inner cylinder (Bil) and stops at a certain point. the ring (BI 12) located in the upper part of the cylinder (BI3), also the telescopic antenna (BII19), which is pushed into the lower part of the shaft (BII7), is telescopically stretched hydraulically, then the primary processes in the tunnel element begin (B ) acceleration of the spacecraft in airless space: electrodes (BII10) are turned on, slightly protruding from the shaft (BII5) and shaft (BII5) also slightly protruding in front of the vessel and funnel input BII18, electrodes (BII10) spray electrons in front of funnel input (BII) 18 which the vessel pulls inwards during the flight, the lamellae (BII15) help to rotate the currents and the electrons enter the primary tunnel of the element (B) during the inward pull and pass through the light tunnel. produced by light sources (BII12) and (C2), which radiate opposite, so in this light field photons excite electrons, and fans (C6) now operate at a lower speed. A spacecraft according to claims 1 to 5, characterized in that the ends of the blades (E17) have electromagnets (C4) and when the winding (B13) is under current, an electromagnetic field is created where the electromagnetic currents are partially amplified, with further By pulling in, the electromagnetic currents from the primary tunnel of the element (B) enter the turbulators (D), where the electromagnetic currents in the electromagnets (D8) and drill accelerators (D7) are amplified and further rotated. cylinder (BI3) and push the spacecraft on electromagnetic waves emitted by a telescopic antenna (BII19) and received by the cylinder (BI3), thus performing two processes in the tunnel (BI3) inside where the solar cells (BI10) are attached : the process of pushing a spacecraft and obtaining electricity for the needs of the spacecraft, while charging the batteries (BII4) in a similar way as for solar power plants. Spacecraft according to claims 1 to 6, characterized in that there are solar cells (BI 10) on the inside of the cylinder (Bil 10), which come into play when the cylinder (Bil) is further lowered along the cylinder (BI3) and with additional solar cells (BI10) we obtain additional electricity, and on the outside of the cylinder (BI3) solar cells (BI 10) are mounted, as well as mounted on a telescopic cylinder (E23), which can be used to obtain electricity from the sun or stars , but if the spacecraft is far away from the stars, electricity is generated only in the secondary tunnels formed by cylinders (BI3), (Bil), and in the four side accelerators (El, EH, Elll and EIV) with cylinders (E23) , when in the extended position and by means of telescopic antennas (BII19) and (E22) with mixed amplified electromagnetic currents and waves, this process performs the processes of pushing the spacecraft and obtaining electricity and charging batteries (BII4). Spacecraft according to Claims 1 to 7, characterized in that hydrogen is obtained from water by electrolysis for the needs of auxiliary electric generators on hydrogen (Bill), and electricity is obtained by solar cells (BI10) and auxiliary electric generators on hydrogen ) in case of failure of the solar cell system (BI10) and other elements crucial for electricity generation. A spacecraft according to claims 1 to 8, characterized in that it lands according to the following procedure: first, the braking processes begin when two side accelerators and guides (El) and (Eli) rotate 180 degrees, the other two (Elll) and (EIV) remain in the same position, then in the primary tunnel of element (B) and the secondary tunnel of element (B) formed by the cylinder (BI3) in the extended position, the thrust processes stop so that the fans (C6), magnets (C4), electrodes (Bil 10), winding (BII13) and turbulators (D) with fans (D6) at rest and when the spacecraft is rotated 180 degrees, the rectifiers (El) and (Eli) return to their original position and thus, all four routers (El - EIV) are facing in the same direction, ie in the direction of braking, then in the primary tunnel of element (B) and in the secondary tunnel of element (B) all previously listed elements start working again and the braking process and space the vessel reaches the planet, orbiting it through the airless space so much time to reach the ideal speed and when this is reached, the telescopic cylinder (E23), telescopic antenna (E22), outer cylinder (Bil) and telescopic antenna Bil 19 begin to return to folding, electrodes (BII10), winding (BII13) , the electromagnets (D8) and the electromagnets (Eli) are stopped, the light sources (E13) and (C2) are switched off, only all the fans (C6, D6, E27 and E15) are still running and when the vessel reaches the appropriate speed it enters the atmosphere and lands vertically at the desired location and does not require a parachute, but brakes and lands in a controlled manner by regulating the speed of all fans (C6, D6, E27 and E15). Spacecraft according to Claims 1 to 9, characterized in that in the middle of the outer cylinder (Bil) there is a spiral (BI2) passing through the entire circumference, through which gas or liquid circulates, thus the outer cylinder (Bil) with a spiral BI2) protects against cosmic radiation element (A), where the crew cabins, which is also a function of the spiral (BI4) in the cylinder jacket (BI3), inner cylinder (BI3) and orings (BI5) and (BI6) on the element (B) ) and the orings (BI7) on the cylinder (BI3) seal the space between the element (B) and the cylinder (Bil), in which there is a vacuum, which is achieved with a vacuum assembly (BI9), which allows us to rotate the element (A) and reduces the noise of the vessel in the atmosphere and the air enters it only in case the crew wants to get out of the spacecraft.