WO2021257002A1

WO2021257002A1 - Spacecraft powered by electromagnetic waves with primary and secondary tunnel for accelerating in the vacuum and generating electricity to propel the craft

Info

Publication number: WO2021257002A1
Application number: PCT/SI2021/000006
Authority: WO
Inventors: Silvano Bizjak
Original assignee: Energetik, Silvano Bizjak S.P.
Priority date: 2020-06-19
Filing date: 2021-06-09
Publication date: 2021-12-23
Also published as: SI26013A

Abstract

The subject-matter of invention is a spacecraft powered by electromagnetic waves with a primary and secondary tunnel for acceleration in the interplanetary, interstellar and intergalactic space and generation of electricity to power the craft. Its advantages are: it is environmentally-friendly, suitable for long-range flights, almost inaudible, and it generates electricity from its own electromagnetic waves. At the launch, it consumes less energy than current spacecrafts. The crew is protected from cosmic radiation. In the space, the Element (A) accommodating the crew and Element (B) are rotating in opposite directions, which enables gravitation in the living space of Element (A) generated by constant rotating, thereby creating centrifugal force that keeps the crew with feet on the floor in their rooms. The craft needs small-size hydrogen-powered electricity generators (BI11) to charge the batteries (BII4) in case of general failure. Optionally, wings of any form, bearing additional solar cells (BI10), may be incorporated in the spacecraft. The modular design of the craft enables that it can be easily disassembled to facilitate maintenance.

Description

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

The subject-matter of invention is a spacecraft propelled by electromagnetic waves with a primary and secondary tunnel for acceleration in the space void of air {vacuum) and generation of electricity to power the craft flying in the atmosphere or interplanetary, interstellar and intergalactic space. The craft features acceleration, turning and braking in the vacuum or in the atmosphere.

The technical problems addressed and solved by this invention include: How to accelerate in a space void of air; how to keep the fuel consumption at the launch low; how to turn and brake the craft in vacuum; how to create artificial gravitation for the crew; how to protect the crew from cosmic radiation; how to reduce the speed before entering the atmosphere and at a landing in the atmosphere without using additional speed braking device like a parachute. Furthermore, it solves the problem of constant acceleration in space void of air.

Technology known today: To overcome the Earth’s gravitation, at the launch and through the atmosphere, spacecrafts are mostly using chemical propulsion (oxygen, hydrogen, and solid fuels, methane, etc.). Ion thrust engines (using gas, like xenon) are used for accelerating the spacecraft in the interplanetary space. With both engines, there is a problem of braking before entering the atmosphere of the target planet. In contrary to the solutions known to date, the invention proposed enables the spacecraft to enter the atmosphere with a reduced speed, not needing a braking parachute for landing. Vertical landing is designed. The spacecraft does not pollute environment and while travelling, noise emission is minimal.

Some additional operating principles used by the craft under the invention have already been described in patents SI9300414 (W09504900A2), SI24404 (WO2014209240 A4), S 124409 (WO2014204412), SI24931 (W02016130093A1) and SI25331

(WO2018111199): e.g. slide transmission of electricity; braking and sealing by means of sealing rings (‘O-Rings’), and fastening by blockers; therefore, repeated description is not necessary.

The patent is described by way of an execution case and by drawings presenting:

Figure 1: Element A - living space in the spacecraft, with magnets and bearings spirally installed in the interior.

Figure 2: Element B with spirally installed magnets, bearings and coils.

Figure 3: Cross section of Element B with a tunnel, axle, funnel-like entry and funnellike exit.

Figure 4: Ventilating fans, bar-shaped carriers and source of light on the axle; visible are also the blockers that form a part of Element B.

Figure 5: Presentation of turbulators located at the exit from the spacecraft: it is shown how they are fastened onto the lower axle, and a display of telescopic aerial Bill 9. Figure 6: display of installation of magnets on turbulators and of grooves or lamellas on the funnel-shaped entry.

Figure 7: Display of installing the ventilating fans and a drill-shaped flow accelerator. Figure 8: Ground plan of turbulators with bar-like carriers and hydraulic blockers in the lower part of the craft at the funnel-shaped exit.

Figure 9: Display of side accelerator and steering device of the craft E.

Figure 10: Ground plan of the craft with all side accelerators and steering device of the craft E.

Figure 11: Display of blockers in the upper part of the craft for the Cylinder BI1 and Telescopic cylinder BI3 with O-rings BI5 and BI7.

Figure 12: Cylinder BI3 in suspended position in the lower part of the craft, with solar cells BI10 and vacuum assembly BI9 and telescopic aerial Bill 9 in extended position. Figure 13: Full view of the spacecraft with all elements A, B, BI1, C, D, E in Bill 9. Figure 14: Full view of the spacecraft with Cylinder BI3 in extended position while building the secondary tunnel with the aerial Bill 9 in extended position.

Concrete reference marks in the drawings stand for the components of the craft under the invention: Element A: Crew’s living space rotates around the Element B and thereby creates artificial gravity for the crew.

Element B: as a stator of the spacecraft and accelerator of photons and electrons toward magnetic turbulators

Element C: Central accelerator with ventilator fans C6, affixed to the axle of the Element B; bar-shaped carriers Cl, source of light C2,

Element D: Turbulators in the lower part of the craft, at the funnel-shaped exit. Element E: Side accelerator and steering device of the craft - this element helps to stabilize the craft at the launch/take-off and turn the craft, as well as to accelerate in the space void of air; it is structured similarly as the Element B with a tunnel for acceleration and funnel-shaped entry and exit.

A1 and Bl: bearings at the funnel-shaped entry.

A2 and B2: magnets located spirally on the funnel-shaped entry and mirror opposite counterparts (of opposite pole and counter-positioned).

A3 and B3: bearings located in front of entrance to tunnel.

A4 and B4: Bearings over the entire rim.

A5 and B5: magnets installed across the whole rim that enable rotation.

A6 and B6: bearings in front of magnets for generating electric power.

A7 and B7: magnets A7 in the centre of the craft, and coil B7, enabling power generation while elements are rotating.

A8 and B8: bearings along the whole rim that enable rotation.

A9 and B9: magnets spirally installed along the whole rim and enabling constant rotation.

A10 and BIO: Bearings along the whole rim in front of funnel-shaped exit.

All and Bll: Bearings at the front of funnel-shaped exit.

A12 and B12: Magnets are spirally counter-positioned over the funnel-shaped exit.

A13 and B13: Bearings in front of funnel-shaped exit.

Bll: External cylinder

BI2: Spirals along the rim of external cylinder Bll.

BI3: Internal cylinder between the external cylinder Bll and Element A BI4: Spiral along the internal cylinder BI3 BI5: Upper O-rings on Element B BI6: Lower O-rings on Element B BI7: O-rings on internal cylinder BI3 BI9: Vacuum assembly

BI10: Solar cells in the interior of cylinder BI3, also installed in the interior of cylinder BI1 and in E23, inside and outside of this cylinder.

Bill: Hydrogen-powered electricity generator.

BI12: Ring on internal side of the cylinder BI3, which blocks the internal cylinder BI3 in the lower part of Element B

Bill: Space for batteries, electronics, coils, electricity generator, telescopic aerial, vacuum assembly and electrodes

BII2: Condenser

BII3: Diode

BII4: Batteries

BII5: Hollow axle installed along the entire tunnel, where tube-shaped supports BII6 are designed and made aerodynamically.

BII6: supports of axle BII5 and BII7, on which cables and electrodes can be installed. BII7: Lower part of axle to which magnetic turbulators are affixed and a telescopic aerial is built-in.

BII8: telescopic bottom supports.

BII9: Bearer of coupling to Element E

BII10: Electrodes, installed along the entire axle to the guard hood Bill 1.

BII11: Cone-shaped guard hood protecting the electrodes on Element B BII12: Source of light that excites electrons.

BII13: Coil

BII15: Lamellas or grooves, to help rotating the flows in Element B.

BII16: Funnel-shaped exit

BII17: Grooves on cone-shaped hood Bill 1.

BII18: Funnel-shaped entry BII19: telescopic aerial.

Cl: Bar-shaped stabilizers that stabilize the hollow axle BII5 in the centre of Element B C2: Source of light on the hollow axle lying opposite to source of light Bill 2. C3: Hydraulic blockers of bar-shaped stabilizers, embedded on the hollow axle and on Element B.

C4: electromagnets at the end of blades on ventilating fans C5: rotor, on which ventilating fans C6 are fastened.

C6: Ventilating fans.

Cl: Magnetic bearings (other bearing types possible, too).

C8: Coil enabling rotation with magnets C9.

C9: Magnets on the rotor.

CIO: Feeding cables with connectors and blockers E8, as shown in Figure 9.

Cll: Support of complete ventilating fan that is installed on the hollow axle BII5.

C12: Ring affixed to the hollow axle BII5 and connected by bar-shaped stabilizers Cl and hydraulic blockers C3 which stabilize the axle BII5 in the centre Dl: Funnel-shaped entrance on turbulators

D2: Hollow axle that bears/supports the ventilating fans D6 and the spiral accelerator D7.

D3: Bar-shaped supports (stabilizers) affixed to Element B in the lower part, on axle BII7.

D4: Rings holding the turbulators with bar-shaped supports D3.

D5: Rings put on the lower axle BII7 that support turbulators.

D6: Ventilating fans affixed to the axle D2.

D7: Spiral accelerators that initiate flow rotation.

D8: Electromagnets installed across the entire turbulator rim, that enable acceleration of electrons and photons in a space void of air; installed spirally.

D9: Slightly bowed grooves that help with flow rotation.

DIO: Feeding cables with connectors and hydraulic blockers E8, as shown in Figure 9. El: Side accelerator and steering device affixed to external cylinder BI1.

Eli: Side accelerator and steering device affixed to external cylinder BI1.

EIII: Side accelerator and steering device affixed to external cylinder BI1.

EIV: Side accelerator and steering device affixed to external cylinder BI1.

El: Ring, support of side accelerators and steering devices El, Eli, EIII, EIV.

E2: Hydraulic blockers of bar-shaped supports E5.

E3: Upper axle on the funnel-shaped entrance Bill 8. E4: Lower axle on expanded exit.

E5: Bar-shaped stabilizers.

E6: Ring in the axle centre, fastened by bar-shaped supports.

E7: Ring in the centre of the lower axle, and turbulators support.

E8: Hydraulic blockers in the axle and Element E.

E9: Tubes routed in a spiral from turbulators E10 to expanded exit, pointing to the direction of enhanced photons flows and excited electrons, which strengthen in the magnetic spiral tubes and generate thrust.

E10: Intake of photons and electrons flows to turbulators.

Ell: Electromagnets with embedded spiral tubes E9.

E12: Electrodes installed in the axle interior E3.

E13: Source of light.

E14: Coil.

E15: Ventilating fans.

E16: Ventilator blades.

E17: Electromagnets at the blade tips.

E18: Cone-shaped guard hood protecting the electrodes on Element E.

E19: Grooves on cone-shaped guard hood.

E20: Grooves on funnel-shaped entrance.

E21: Exit from turbulators.

E22: Telescopic aerial, pushed to the lower part of axle E4.

E23: Telescopic cylinder.

E24: Spiral running along one half of cylinder E23.

E25: Blockers.

E26: Holes to block the cylinder E23.

E27: Ventilating fans in turbulators. Spacecraft is powered by electricity utilizing electric power, light and magnets for propelling. It is composed of the following basic elements: the living space A, which is built externally into the element containing the acceleration tunnel B and BII, which is vacuumized and coated by light-reflecting material. Contact with central accelerator with photons and electrons C, which comprises ventilating fans C6 affixed to the axle of element B, bar-shaped supports Cl, source of light C2 in which partial flow-acceleration processes take place towards magnetic turbulators D, located in the lower part of the spacecraft, whilst side accelerators and steering devices E are affixed to the craft on each side, functioning to turn and accelerate the craft in the space void of air. The craft may also have wings of any shape, modularly dismountable.

Before the spacecraft is launched, it stands vertically, all other telescopic elements except bottom supports BII8 are folded in, that is: external cylinder BII, internal cylinder BI3 and also telescopic aerial BII 19, which is telescopically pushed into the lower part of the axle BII7. When the launch from the ground in the atmosphere begins, all the lateral accelerators and steering devices El, Eli, EIII and EIV that are affixed to the external cylinder BII on the bearers BII9, which can still rotate, are turned to the ground. Also, the lateral accelerators and steering devices El, Eli, EIII and EIV are folded in. The telescopic aerial E22 is pushed to the lower part of axle E4. The cylinder E23 is covered from external and internal side with solar cells BI10. Between internal and external solar cells BII 10 is installed the spiral E24, in which the gas or liquid is flowing. The spiral E24 is used to cool or heat the cylinder E23, when necessary. In the lower element E, we switch on all the four ventilating fans E27 in the turbulators E10, whilst electromagnets El 1 are disengaged. After that, we switch on the ventilator El 5 in the primary tunnel of element E. Other elements: electrodes E12, source of light E13, electromagnets Ell, electromagnets at blade tips E17 and the coil E14 are disengaged. While the ventilating fans E27 in turbulators D are engaged (in the operating phase), they stabilise the spacecraft and help defying the gravity. In the lower primary tunnel of the element B, we switch on the ventilating fans D6 in turbulators D and lastly, the ventilating fans C6 in the upper part of the primary tunnel of element B. After that, all the remaining elements are in the lower primary tunnel B: electrodes BII 10, coil Bill 3, electromagnets D8, electromagnets at blade tips C4, source of light BII 12 and the source of light C2 on the axle BII5, are disengaged during the spacecraft journey in the atmosphere.

When the spacecraft takes off and overcomes the gravity of the planet, it reaches the interplanetary space. There start acceleration processes on electromagnetic waves. We start engaging individual elements in the following order of sequence: first, the internal cylinder BI3 slides along the spacecraft between the internal cylinder BI1 and stops at a certain point, blocked with the ring BI12 that is located in the upper part of cylinder BI3. Also, the telescopic aerial Bill 9, which is pushed to the lower part of axle BII7, is extended telescopically by hydraulics. This is followed by primary processes in the tunnel of element B - acceleration of the spacecraft in the interplanetary space. Electrodes BII10 engage, which slightly rise from the axle BII5, and the axle BII5 engages, which also protrudes (stands out) slightly in front of the spacecraft and of the ftmnel-shaped entrance Bill 8. The electrodes BII10 emit electrons in front of the funnel-shaped entrance Bill 8, and the spacecraft sucks them inside during the flight. Lamellas Bill 5 help rotating the flows, and electrons are sucked into the primary tunnel of element B and go through the field of light created by the sources of light Bill 2 and C2. Both light sources radiate in opposite directions. In this light field, the photons excite the electrons (See Figure 13). Ventilating fans C6 are now operating at a lower speed. Electromagnets C4 are installed at the blade tips El 7, and electromagnetic field is generated when the coil B13 is under the current, where electromagnetic flows get partly strengthened. In the course of subsequent inward drag process, the electromagnetic flows from primary tunnel of element B get into turbulators D, where electromagnetic flows in electromagnets D8 and the spiral accelerators D7 intensify and additionally rotate faster. The strengthened electromagnetic flows get into the telescopically extended secondary tunnel of the internal cylinder BI3, and push the spacecraft on electromagnetic waves which are emitted by the telescopic aerial Bill 9, and the cylinder BI3 is receiving them. Accordingly, two processes are going on inside this tunnel BI3, where the solar cells BI10 are installed: the thrust of the spacecraft, and the electricity-generating process for the needs of the spacecraft, concurrently charging the batteries BII4 similarly as in solar power plants. On the internal side of cylinder BI1 are located the solar cells BI10, which are used when the cylinder BI1 additionally descends along the cylinder BI3 and thus additionally prolongs the secondary tunnel BI3, enabling to generate additional electric energy by internal solar cells BI10.

In the coat of cylinder BI1 is installed the spiral B|2, along which gas or fluid is conducted to protect the crew in the living space of element A against cosmic radiation. The spiral BI4 in the coat of cylinder BI3 has the same function.

Solar cells BI10 are affixed on the external side of the cylinder BI3 and to the telescopic cylinder E23, which can generate electricity from the sun or stars. If the spacecraft is very far from the stars, electric energy can be generated only in the secondary tunnels formed by the cylinders BI3, BI1, and in the four lateral accelerators El, Eli, EIII and EIV with cylinders E23 while these are in extended (stretched) position, and by telescopic aerials Bill 9 and E22, with mixed intensified electromagnetic flows and waves. That is how the thrust of the spacecraft and electricity-generating process, as well as charging of batteries BII4 take place.

For the needs of auxiliary hydrogen-powered electricity generator Bill, hydrogen is gained from the water by electrolysis. The spacecraft generates electricity by solar cells BI10 and by auxiliary hydrogen-powered electricity generators Bill in the event of failure on the solar cell system BI10 and (failure) of other elements of key importance for the generation of electricity.

Spacecraft landing: Braking processes start before the spacecraft achieves its goal. At that time, the two lateral accelerators and steering devices El and Eli (Figure 10) rotate by 180 degrees. The other two EIII and EIV remain in the same position. The steering devices in pairs are pushing in opposite directions to turn the spacecraft. In the primary tunnel of element B and in the secondary tunnel of element B, formed by the cylinder BI3 in the extended position, the thrust processes stop when the ventilating fans C6, electromagnets C4, electrodes BII10, coil Bill 3 and turbulators D with ventilating fans D6 stop and remain in a standstill phase. When the entire spacecraft is turned by 180°, 10 the steering devices El and Eli return to their primary position and accordingly, all the four steering devices (El — EIV) are facing in the same direction - i.e. in the direction of braking. All the above listed elements engage again in the primary tunnel of element B and in the secondary tunnel of element B, formed by the cylinder BI3 in extended position, and the braking process begins. When the spacecraft reaches the goal (the earth, moon, other planet, ...), it circulates around the planet for as long as necessary to reach the ideal speed; once that speed is reached, the telescopic cylinder E23, telescopic aerial E22, external cylinder BI1 and telescopic aerial Bill 9 begin to return into the folded-in status. Electrodes BII10, coil Bill 3, electromagnets D8 and electromagnets El 1 are brought to a stop /standstill. Also, the sources of light El 3 and C2 disengage. Only all the ventilating fans C6, D6, E27 and El 5 are operating. The speed of these ventilating fans is controlled by electronics. Once the spacecraft has reached an eligible speed, it enters the atmosphere and lands vertically at the desired location without needing a parachute: it brakes and lands in a controlled mode, by speed regulation of all ventilating fans C6, D6, E27 and El 5.

In the middle of external cylinder BI1 is installed a spiral BI2 across the entire rim, in which gas or fluid is circulating. In that way, the external cylinder BI1 with the spiral BI2 protects the element A (accommodating the crew cabin) against cosmic radiation. The internal cylinder BI3 and the O-rings BI5 and BI6 on the element B, and the O- rings BI7 on the cylinder BI3 seal the space between element B and cylinder BI1. In that space is vacuum, which is achieved by the vacuum assembly BI9. Vacuum facilitates the rotation of element A and reduces the noisiness of spacecraft in the atmosphere. Air gets into that space only when the crew wishes to exit from the spacecraft.

The advantages of this spacecraft are: the spacecraft will not pollute the environment, it will be adequate for long-distance flights; it is almost noiseless, electricity will be generated from its own electromagnetic waves, therefore, the craft will not need a nuclear reactor or ionic engine that can only store a limited quantity of fuel. It will be fed by own electromagnetic waves, irrespective of exposure to sunshine or stars. At the launch, it will consume less energy than present-day spacecrafts. The crew will be protected from cosmic radiation. In the interplanetary space, the Elements A and B are rotating in opposite directions, which enables gravitation in the living space of Element A generated by constant rotating, thereby creating centrifugal force that keeps the crew with feet on the floor in their room. The craft will need small-size hydrogen-powered electricity generators Bill to charge the batteries BII4 in case of general failure. Electricity generators Bill will engage only at the take-off. Once the craft has overcome the planet’s gravity, these generators will disengage. Optionally, wings of any form, bearing additional solar cells BI10, may be incorporated in the spacecraft. The modular design of the craft enables that it can be easily disassembled to facilitate maintenance.

Claims

PATENT CLAIMS

1. The spacecraft powered by electromagnetic waves with a primary and secondary tunnel for acceleration in the space void of air (interplanetary, interstellar and intergalactic space) and generation of electricity to power the craft, characterized by the fact that it is powered by electricity utilizing electric power, light and magnets for propelling, consisting of the basic elements: the living space (A), which is built externally into the element containing the acceleration tunnel (B and BII), which is vacuumized and coated by light-reflecting material; elements (A) and (B) are rotating in the interplanetary space in opposite directions, which enables gravitation in the living space of element (A) generated by constant rotating; element (B) is then in contact with central accelerator with photons and electrons (C), which comprises ventilating fans (C6) affixed to the axle of element (B), bar-shaped supports (Cl), source of light (C2) in which partial flow-acceleration processes take place towards magnetic turbulators (D), located in the lower part of the spacecraft, whilst lateral accelerators and steering devices (E) are affixed to the craft on each side, functioning to turn and accelerate the craft in the space void of air; a part of element (E) is the cylinder (E23) that is covered from external and internal side with solar cells (BI10), between which the spiral (E24) is installed in which the gas or liquid is flowing and used to cool or heat the cylinder (E23) when necessary; wings of any form may be incorporated in the spacecraft; modular design.

2. The spacecraft under claim 1, characterized by the fact that before taking off, it stands vertically, all other telescopic elements except bottom supports (BII8) are folded in, that is: external cylinder (BII), internal cylinder (BI3) and also telescopic aerial (BII 19), which is telescopically pushed into the lower part of the axle (BII7).

3. The spacecraft under claims 1 and 2, characterized by the fact that when the take-off from the ground in the atmosphere begins, all the lateral accelerators and steering devices (El, Eli, EIII and EIV) that are affixed to the external cylinder (BI1) on the bearers (BII9) are turned to the ground; the lateral accelerators and steering devices (El, Eli, EIII and EIV) are folded in, telescopic aerial (E22) is pushed into the lower part of the axle (E4); in the lower element (E) we switch on all the four ventilating fans (E27) in turbulators (E10), the electromagnets (El 1) are disengaged, then we engage ventilating fan (El 5) in the primary tunnel of element (E), whilst the remaining elements: electrodes (El 2), source of light (El 3), electromagnets (Ell), electromagnets at blade tips (El 7) and the coil (El 4) are disengaged.

4. The spacecraft under claims 1 to 3, characterized by the fact that when ventilating fans (E27) in turbulators (D) are engaged (in the operating phase), they stabilise the spacecraft and help defying gravity, then we switch on in the lower primary tunnel of element (B) the ventilating fans (D6) in turbulators (D) and as last, the ventilating fans (C6) in the upper part of the primary tunnel of element (B).

5. The spacecraft under claims 1 to 4, characterized by the fact that when it takes off and overcomes the gravity of the planet, the acceleration processes on electromagnetic waves are commenced, therefore we start engaging individual elements in the following order of sequence: First, the internal cylinder (BI3) slides along the spacecraft between the internal cylinder (BI1) and stops at a certain point, blocked with the ring (BI12) located in the upper part of cylinder (BI3), also telescopic aerial (Bill 9), which is telescopically pushed into the lower part of the axle (BII7), is telescopically extended by hydraulics, and then the primary processes in the tunnel of element (B) begin - acceleration of the spacecraft in the airless interplanetary space: electrodes (BII10) engage, which slightly rise from the axle (BII5), and the axle (BII5) engages, which also protrudes (stands out) slightly in front of the spacecraft and of the funnel-shaped entrance (Bill 8), and the electrodes (BII10) emit electrons in front of the funnel-shaped entry (Bill 8), and the spacecraft sucks them inside during the flight; lamellas (Bill 5) help rotating the flows, and electrons are sucked into the primary tunnel of element (B) and go through the field of light created by the sources of light (Bill 2) and (C2) which radiate in contrary directions, which is why the photons excite the electrons in this light field, and ventilating fans (C6) are now operating at a lower speed.

6. The spacecraft under claims 1 to 5, characterized by the fact that electromagnets (C4) are installed at blade tips (El 7) and an electromagnetic field is generated when the coil (B13) is under current, where electromagnetic flows get partly strengthened; in the course of subsequent inward drag process, the electromagnetic flows from primary tunnel of element (B) get into turbulators (D), where electromagnetic flows in electromagnets (D8) and the spiral accelerators (D7) intensify and additionally get rotating, and these strengthened electromagnetic flows get into the telescopically extended secondary tunnel of the internal cylinder (BI3) and push the spacecraft on electromagnetic waves which are emitted by the telescopic aerial (Bill 9), and the cylinder (BI3) is receiving them; in the course of which two processes take place inside the tunnel (BI3) where solar cells (BI10) are installed: the thrust of the spacecraft, and the electricity-generating process for the needs of the spacecraft, concurrently charging the batteries (BII4) similarly as in solar power plants.

7. The spacecraft under claims 1 to 6, characterized by the fact that solar cells (BI10) are installed inside the cylinder (B|l) which are used when the cylinder (BI1) additionally descends along the cylinder (BI3) enabling to generate additional electric energy by internal solar cells (BII10); solar cells (BI10) are also installed on the external side of the cylinder (BI3) and on the telescopic cylinder (E23), which are used to generate electricity from the sun and stars; if the spacecraft is rather far from stars, electric energy can be generated only in the secondary tunnels formed by the cylinders (BI3, BI1), and in the four lateral accelerators (El, Eli, EIII and EIV) with cylinders (E23) while these are in extended position, and by telescopic aerials (Bill 9 and E22), with mixed intensified electromagnetic flows and waves; this process is instrumental to effect the thrust of the spacecraft and electricity-generating process, as well as charging of batteries (BII4).

8. The spacecraft under claims 1 to 7, characterized by the fact that for the needs of auxiliary hydrogen-powered electricity generator (BI11), hydrogen is gained from the water by electrolysis, and electricity is generated by solar cells (BI10) and by auxiliary hydrogen-powered electricity generator (BI11) in the event of failure on the solar cell system (BI10) and (failure) of other vital elements for the generation of electricity.

9. The spacecraft under claims 1 to 8, characterized by the fact that its landing process is as follows: braking processes start first when two lateral accelerators and steering devices (El) and (Eli) rotate by 180 degrees, the other two (EIII) and (EIV) remain in the same position; after that, in the primary tunnel of element (B) and in the secondary tunnel of element (B) formed by the cylinder (BI3) in the extended position, the thrust processes stop when the ventilating fans (C6), electromagnets (C4), electrodes (BII10), coil (Bill 3) and turbulators (D) with ventilating fans (D6) stop and remain in a standstill phase; and when the entire spacecraft is turned by 180 degrees, the steering devices (El) and (Eli) return to their primary position and accordingly, all the four steering devices (El — EIV) are facing in the same direction - i.e. in the direction of braking; then, in the primary tunnel of element (B) and in the secondary tunnel of element (B) all the above listed elements engage again, the braking process begins and the spacecraft reaches the planet, circulates around it for as long as necessary to reach the ideal speed; once that speed is reached, the telescopic cylinder (E23), telescopic aerial (E22), external cylinder (BI1) and telescopic aerial (Bill 9) begin to return into the folded-in status, the electrodes (BII10), coil (BII13), electromagnets (D8) and electromagnets (El 1) stop, the sources of light (El 3) and (C2) are switched off, with only all the ventilating fans (C6, D6, E27 and El 5) operating, and when the spacecraft has reached an eligible speed, it enters the atmosphere and lands vertically at the desired location without needing a parachute, as it brakes and lands in a controlled mode, by speed regulation of all ventilating fans (C6, D6, E27 and El 5).

10. The spacecraft under claims 1 to 9, characterized by the fact that in the middle of external cylinder (BI1) is installed a spiral (BI2) across the entire rim, in which gas or fluid is circulating; in that way, the external cylinder (BI1) with the spiral (BI2) protects the element (A) accommodating the crew cabin against cosmic radiation, which is also the function of the spiral (BI4) in the coat of cylinder (BI3); the internal cylinder (BI3) and the O-rings (BI5 and BI6) on the element (B), and the O- rings (BI7) on the cylinder (BI3) seal the space between element (B) and cylinder (BI1) under vacuum, achieved by the vacuum assembly (BI9) to facilitate the rotation of element (A) and reduce the noisiness of spacecraft in the atmosphere; air gets into that space only when the crew wishes to exit from the spacecraft.