JP2022120862A - Differential pressure type (space) propulsion and stay-in-air (stay-in-space) system mainly applying imbalance of force - Google Patents

Abstract

To generally achieve a space propulsion technology that is far safer than extremely dangerous rocket propulsion of the existing space propulsion technology.SOLUTION: To put it very briefly, not the physical phenomenon based on the established theoretical mathematical formula: F1+(-)F2=0, F1=(-)F2, which is the basis of a rocket engine, applying the physical phenomenon based on a new theoretical mathematical formula: F1+(-)F1=0, F2+(-)F2=0, F1≠F2, in a closed fluid system (system of a hollow body and various fluids mixed in the body), various types of flowable substances and fluids (including dangerous rocket liquid fuel, etc.) are intentionally circulated in the hollow body at all times, and while causing a corresponding pressure (internal pressure) difference around the opposite ends of the body, just like the buoyance (for gravity reduction) arising from a pressure (external pressure) difference in the earth sphere, especially in the space sphere, a (space propulsion) effect (named superpower) arising from the pressure (internal pressure) difference continues to be generated and generated naturally.SELECTED DRAWING: Figure 1

Description

The present invention relates primarily to aerospace propulsion technology and the like.

First of all, the fundamental (rudimentary) basic principle of thrust generation of this pressure (internal pressure) differential propulsion system (the universal principle of physics that is still unknown) is reconsidered, and it is a universal standard language ( In English (with alphanumeric characters), it is generally described as follows.

~A new frontier of physical (space) science based mainly on Newton's […] laws of motion (fused just the existing dynamics & statics)~

Principally, fundamental principle of modern spacecraft (rocket) propulsion has been based on Newton's third law of motion: action and reaction by decisive (immovable) definition as follows.

For every action, there is an equal and opposite reaction.

In other words,
if object A (1st body) exerts a force on object B (2nd body),
then the second body simultaneously exerts a force equal in magnitude and opposite in direction on the first body. (by NASA etc)

But, this description of the above forces equation (without dynamic external force) on the two different bodies would have been quite often misunderstood as static equilibrium of forces upon the one (undifferent) body.

*Note : It requires close attention that it couldn't have been settled whether the object would have remained at rest or in uniform motion only with the fixed formula implicitly indicated equilibrium of forces in the statics : F = 0 (F1 + -F2 = 0).
---However, the above object's alternative physical phenomenon of “at rest” or “in motion” could (should) be so easily solved (selected) by the new (unknown) next equation [F1 + -.. = 0]… .

Because the second (2nd) body has just returned naturally, equally the action force from the first body to the same (1st) body.
So, it should be properly interpreted that a spontaneous action force by the 2nd ^body itself has not been included in the interaction* between the two bodies.

For example, when a moving object 1 collides against an object 2 at rest with no action force spontaneously by itself, the dynamic body's force (F1) and the static body's force (F2) are obviously unbalanced at the collision (despite being established by the existing action reaction law as if F2 which ought to be just F0 with its (zero) velocity is the same as a standard for F1's value), even though the momentum of the two bodies would have completely conserved before and after the collision... .

*Note: The object 2 at rest has been certainly (undoubtedly) moved by the (external) force: F1, not the (internal) force: F2 at that collision.
And so, each basic equation related to the momentum conservation in this case is…

m1v1'- m1v1 = F1 (= dp1/dt) as to the object 1,
m2v2' - m2v2 = -F1 (= dp2/dt) as to the object 2,
(not always m2v2' - m2v2 = -F2 = dp2/dt)
--Because it's been limited to equilibrium of forces with F1 only, if it is just -F2…

**As for the following fundamental equation of the momentum conservation,
m1v1 + m2v2 = m1v1' + m2v2'
it could have been merely established by the (balanced) force in common: [F1=(-)F2].
But, this is nothing short of a blind spot for disregarding the true value of that (unbalanced) force: [F1≠(-)F2]....

**As for a pair of the above forces (F1&F2) acting on the two interacting objects, F2 should be a fictitious (inertial) force, not a real force, in case of the standard for F1's value, regardless of any (non) inertial frame of reference….

After all, in the background of being quite capable of having a misunderstanding as if an action force of one body [A] & an action (not a reaction) force of the other body [B] had been equal at all in consideration of such an action-reaction between the same bodies [A & B], it is not too much to say that it has been confused by the definitional fixed word: “inter-Action” (like as action-action against action-reaction) and also , exactly the same formula [F1+(-)F2=0] for the force-equation (on one body) and the action-reaction (on two bodies) so far….

Therefore, the mathematical simple formula structure mainly (especially) in case of interaction with A&B's (unbalanced) action forces : (F1≠F2, F1> F2 or F1 < F2) should be corrected as below.

F1 + (-)F1 = 0 F2 + (-)F2 = 0
(not F1 + -F2 = F net = 0 as Force equation)

F1 : an action force that a body [A] itself exerts.
(-)F1: a reaction force that the same body [A] is exerted.
F2 : an action force that a body [B] itself exerts.
(-)F2: a reaction force that the same body [B] is exerted.

Thus it is better (best) for the true formula of the action-reaction regarding it as force equation on each body, not both bodies, in case of being a difference (unbalance) between each action force of the interaction.

[The revised edition of the Newton's third law]
(new) Third law
When one body exerts an action force on a second body, the first body simultaneously is exerted with a reaction force equal in magnitude and opposite in direction on the 1st body from the second body (whether an action force by the 2nd body itself is ^exerted or not).
And/or,
One body which exerts an action force to the 2nd ^body is simultaneously, equally reacted as (a kind of) reflection of the action force by the 1st ^body itself, not the other (another) force by the 2nd ^body .

And also,
For every action (force) by one object ((not by the two objects of interaction)) in nature there is an equal and opposite reaction (force) to its own object ((not to a pair of those objects with different forces)) .

~~~
By the way, the law of momentum conservation which the total momentum is constant in a closed system has been implied by the action reaction principle and also it is a synonym for Newton's first law that the velocity of the object is constant if the net force is zero.

F1 + -F2 = (Fnet) = 0 F1 = (-)F2
The above formula(s) shows only an object at rest in an inertial frame of reference.
This is still incomplete as to the same formula only compared to the next formula (which could have expressed synchronously both states of the object at rest as well as uniform motion).

F1 + (-)F1 = 0 and/or F2 + (-)F2 = 0 F1≠F2 (F1> F2 or F1 < F2)
The above formula could indicate not only an object at rest, but also uniform motion, because of expressing a kind of synchronized physical phenomenon applying a principle of superposition in physics (quantum mechanics).

The superposition could have been defined by two simple properties; additivity and homogeneity as follows.

Additivity F (x + y) = F (x) + F (y) [F (x, y) = x + y (= 0)]
Homogeneity F(ax) = aF(x) [= F(ay) = aF(y) = 0]
for scalar a. (F is a function)
x = F1 + (-)F1 (= 0) = F2 + (-)F2 = y
(F1&F2 are forces)

In conclusion, the following theorem(s) could have been proven really in accordance with Newton's second law of motion (F=ma) which comes into effect (force) from the inequality (no equilibrium) of the action forces produced at the same time (moment) and a new unique concept for a closed [fluid] system on a frontier of modern physics (space science) would have been defined as below....

[The Zeroth Law of Motion]
Even if there is no external forces (= 0) outside of the closed system, it could turn one object (a united body) from rest to (uniform) motion by unbalanced forces on each object of inter-action spontaneously without the movement of the center of mass (balance), regarding just a united spot of the mutual objects each other as that zero point (the starting point of the uniform motion)….

[The law of non-conservation of momentum]
Especially in the closed fluid system device which has included a flowable substance in one hollow body, the momentum could not be conserved, as long as inner force (not internal force against external force of interaction) by internal pressure difference between both sides of the same hollow body has been exerted mainly in (outer) space, according to the principle of buoyancy which has justly produced buoyant force by external pressure difference between the top & bottom of a cube in the water of Earth….

Note1 : The above momentum in closed system is conserved only setting a standard of one force value of interaction in case of F1≠F2.
Note2 : Bernoulli's principle in fluid dynamics is not always based on the law of momentum conservation, even though it corresponds to the law of conservation of energy.
Note3 : Although total pressure of dynamic pressure and static pressure is usually constant in the Bernoulli's equation (regardless of an open or a closed system), it could never have been conserved in the closed fluid system devices which would have enabled to store up (potential ) energy with non-steady flowable fluid (not the ideal = perfect fluid).

The buoyant force (= weight of displaced fluid) is equal to net force by the external pressure difference (see below).

(buoyancy) F = [eP2-eP1]*S
eP1: (external) Pressure which fluid pushes down to the top of the cube from the outside of the one body (the downward force on the cube)
eP2: (external) Pressure which fluid pushes up to the bottom of the cube from the outside of the one body (the upward force on the cube)
S: An area of the (exterior) surface upon the net force by the (external) pressure difference….

Then, substituting the next formula : [P = p0 + phg] of pressure in fluids in the atmosphere for P1 & P2 on the above formula, the buoyant force is described as below.

F = pVg (F = mg)
p: density of the fluid V: volume of the cube g: gravitational acceleration

Here, just in case of taking F1 & F2 for each action force by the fluid on P1 and P2, it may replace (interchange) their reaction forces (-F1 & -F2) equally with (apparent) action forces by the same cube( 's both insides).

That means (indicates) the above forces which have been effective from the inside to the outside of that cube (as a kind of the hollow body).

So, pouring some fluid body appropriately into the above hollow body and producing pressure (unbalanced) force on fluid dynamics, not fluid statics, in some way (by certain methods), its body would (should) be able to be active by itself as a matter of course.

Therefore, the hollow body in the closed fluid system could surely be moved by the inner net force (named newly ”super-force”) of the internal pressure difference between both sides of the same body, not by the reaction force….

Super force : sF = [iP2-iP1]*S (= ma)
iP1: (internal) Pressure which fluid in a hollow body pushes backward to one side (an inner wall) of the same body (the backward force on the united body with the fluid in case of iP2 > iP1)
iP2: (internal) Pressure which fluid in a hollow body pushes forward to the other side (an inner wall) of the same body (the forward force on the united body with the fluid in case of iP2 > iP1)
S: An area of the (inner) surface upon the net force by the (internal) pressure difference….
m: Total (gross) mass of the united body with the fluid (etc)

Moreover, when the fluid is circulated in the hollow body repeatedly (many times), causing the pressure difference on the both sides of the same body, the one united (hollow) body would have been able to exert great-est power (the super -er force) with super high speed (of light) especially in the zero gravity space….

And in addition to that, this system device is the safest because of no rocket fuel and so forth.

*Needless to say, the superer force is distinguished from “super force” as unified force in a theory of everything.

[The supplement]
EM drive which really working of its thruster has been confirmed with engine tests by NASA etc has never violated the law of conservation of momentum, just applying that formula : F1 + (-)F1 = 0 and/or F2 + (-)F2 = 0, F1≠F2 (F1> F2 or F1 < F2).

And the driving device which belongs to a closed fluid system on account of including a kind of flowable substance : a photon(s) of an electromagnetic wave(s) inside its device as a closed container could have been propelled by net (unbalanced) force on the internal pressure difference, not the reaction force.

In summary, the above existing device has particularly different size as to each side (both areas of the inner surfaces on contact with the photon) of its hollow body, and therefore, the pressure difference between the both sides of the same body has been caused Mathematically (necessarily).

P1 ≠ P2 P1 = F/A1, P2 = F/A2 A1 ≠ A2

~~~
Super Power Drive that exerts greater (greatest) power extraordinarily, incomparably than the EM drive which is said that it could get us in 4 hours to the moon has been already invented with brand-new several smarter ways (unique smartest methods) by this theorist (the inventor).

The above further information of the SPD is mostly as described in these Japanese documents hereinto….

Especially, the space(craft) propulsion force with a lot of impulses by continuous circulation of the fluids sustainably causing the pressure difference will be able to bring about ultra high speed (semi-light speed) indeed to a brand-new unique spaceship (newly named "Super-Starship") with the super power drive engine, even the same one in the megaton range....

And also, just in case of (simultaneously) using super-er force (power) controllers and direction changing devices and so on, it could have really made the above spaceship stay at a (fixed) point in the (outer)space.. ..

Therefore, the existing artificial satellites etc (which might be turned into space debris) required for orbiting around the earth will become unnecessary (obsolete) after this....

Furthermore, according to the new space (and the like), it would (should) be able to achieve early realization of mainly Space Elevator, utilizing a flexible cable (space tether) etc with a very short length, not so long length ( height) beyond the geostationary orbit, ie, that means it's good enough for currently available materials (such as Kevlar etc), without mass production (difficultly manufacturing) of carbon nanotubes (CNTs)....and so forth.

<Supplement>
In general, it is known that the total pressure in any pump/line (whether open or closed) is constant according to the following formula, even if the flow path and flow velocity are changed: ing.

Total pressure (total pressure) = static pressure + dynamic pressure
P0 = p + qq = 1/2pv2
p + 1/2pv2 = P0 (= constant)

However, in the above formula, especially from Bernoulli's theorem (mainly dealing with ideal fluids such as incompressibility), the numerical value of the potential energy is canceled (ignored), so even in a closed fluid system Even so, if we take in potential energy that can be converted to kinetic energy in a timely manner (immediately), we can pressurize or depressurize while (intentionally and locally) compressing the gas. The object itself (with a height difference, etc.) can inadvertently become propellable.

@In modern physics, in terms of the concept of "system", the (space) propellant invention belonging to the undefined "closed fluid system" has already been made by the applicant. , to some extent, have been made public, but in general, the "laws of nature" referred to in Article 2 of the Patent Act, that is, the established physical laws of natural science (especially the conventional Newtonian mechanics and motion, In light of the law), it must be said that it has been contrary to the firm (immovable) law of action and reaction [F1 + -F2 = 0] for a long time. It was as if they stubbornly considered that they did not have the usefulness (industrial applicability) of the main US patent requirements, etc. As long as it has been acquiesced (ignored) for a long time like incompetence), the universe that can be said to be "publicly known" regarding the exclusion of patent requirements, as defined in Article 29, Paragraphs 1 to 3, etc. of the Patent Law It was not a substitute for equipment, that is, it was not subject to the category of "invention" using the law of nature (law) defined in Article 2 of the same Patent Act, etc. It's up to you.

(if necessary) will be presented later.

(if necessary) will be presented later.

In addition to the common realization of space propulsion technology that is far (by orders of magnitude) more efficient (and as safe as possible) than rocket propulsion, which is the mainstream of existing space propulsion technology (which is extremely dangerous), given pressure (Internal pressure) Differential (space) propulsion equipment, etc., will be substantially completed with better propulsion efficiency by several steps.

Once again, in order to firmly demonstrate the validity of the alphamathematical propulsion technology theory in the above-mentioned pressure (internal pressure) differential space propulsion system, the fixed theoretical formula that is the basis of the rocket engine is roughly: A new theoretical formula, not a physical phenomenon based on F1+(-)F2=0, F1=(-)F2 (a kind of force balance): F1+(-)F1=0= F2+( -) Applying natural phenomena based on F2, F1 ≠ F2 (a kind of force imbalance), a closed fluid system (a system in which various fluids are mixed in the hollow body and its body) at any time In addition, in the same hollow body, various types of fluid substances and fluids (including completely unnecessary mixtures and liquids, such as dangerous rocket liquid fuel) are intentionally circulated, and around both ends of the body, While creating a considerable pressure (internal pressure) difference, just like the buoyancy (for gravity reduction) resulting from the pressure (external pressure) difference in the earth sphere, especially in the space sphere, from the pressure (internal pressure) difference It is enough to continue to generate and generate the effect (for space propulsion) (named superpower) by itself... and so on.
In particular, in order to manufacture improved products (inventions) that are significantly superior to the conventional (applicant's own) devised products, etc. In the hollow body (in which more than one kind of fluid is inserted) belonging to the system, the strong wind (wind force) etc. blown out from the main fan for propulsion (advance) mainly arranged in the upper center (front part) A pressure (internal pressure) differential propulsion system that uses an air barrier device to reduce the backward force (downward force) generated by pushing the inner wall of the rear) was devised. In the case of a dedicated container that mainly contains gas etc., the action of the air barrier can suppress the rearward or downward force applied to the rear wall or lower wall (inner wall) of the propellant body accordingly, but the main body When the air circulates continuously from the rear (lower) to the front (upper) of the body, inevitably, small-scale turbulence ( Along with the local generation of vortex flow), the main air particles naturally push a part of the curved rear surface (lower surface) along the oblique direction and move toward the front surface (upper surface). Since there was a tendency to apply force), first, in order to make the flow of the fluid (gas) smoother, the air passage for main propulsion (route along the vertical direction) and several stages (tiered type) Each air passage for the air barrier (horizontal route) is accompanied by an air tank that secures the required amount of air, and after dividing it appropriately, the main (vertical direction) propulsion route is used sequentially. Regarding the air circulation, once the strong wind blows down, the downdraft region that blows down the strong winds is bypassed to the updraft region on the opposite side through the horizontal air path (air bypass). Also, due to the downward injection of the main propulsion fans during operation, the air suction effect upwards through the (half) torus-shaped air pipes and air tubes on the connection (the blades of the adjacent main fans In order to prevent idling, it is possible to separately adjust the speed of the ventilation, etc., by inserting a rectifying plate that has many small holes in the ventilation port and is empty, in advance, the area of the top surface is made as large as possible. By temporarily accumulating the air being blown in the top half, the majority of the air particles of this propellant are , without touching the bottom surface of the body, that is, without pushing the bottom surface of the body (in other words, For example, without applying a descending force), it is possible to suck it up all at once (even synchronously). In general, considering its basic shape and basic simple structure, first, prepare a plurality of (relatively large size) floating ring-like circular ones, and then sequentially Place an appropriate amount of fluid (gas) in a container, and partially (locally ).
In addition, unless the air particles (most of them) that act as the propellant (assuming that the fluid in the system is gas only) are those that push the lower surface (inner surface) of the main body and generate downward force, In calculating the thrust-to-weight ratio, it is not necessary to add the total weight of the air particles (excluding the part of the weight roughly calculated from the mass of the gas in contact with the lower surface of the main body) to the total weight of the main body. If the gas contains water vapor more than necessary, it should be supplemented in advance that it is desirable to generate an appropriate amount of air flow in a state where the saturated vapor pressure is not reached as much as possible. .

First and foremost, the operation of this space propulsion device (including various equipment such as air circulation type) can constantly generate In the case of thrust with repeated impulses, especially in the zero-gravity space of the outer space, it brings about a really ultra-high speed (quasi-light speed), and also the same device, direction change device, position angle sensor, etc. If you make full use of it, this spacecraft itself can stay in space at a fixed point in space, no, it can stay in space without needing to go around the earth. Satellites, etc., are unnecessary, and by applying the holding power and reinforcing power of staying in the air and staying in the air, the following physical work related to the construction of various (composite) structures is generally performed. In other words, by effectively and efficiently diverting it to a lifting force that tries to pull a predetermined object up, a cable (tether) that transcends even a geostationary orbit far away from the earth. , without needing to extend endlessly, as mentioned above, space elevators etc. ( The early realization of new (new) space structures will generally be achieved, and so on.

Later, it will be described in the procedure amendment.

Later, it will be described in the procedure amendment.

A simplified diagram showing a basic (elementary) example of a (thought) experiment that shows the validity of this theory (new mathematics). * If necessary, we will present Figure 2 and other figures later. As a precaution, in order to avoid illegal plagiarism and plagiarism of patents, designs, etc. etc., if still necessary, this does not apply).

Claims (9)

A closed fluid system (a closed body and various fluids in it: gas and/or liquid, etc.) is calculated by a unique calculation program in a dedicated or general-purpose computer, etc. Based on the numerical data of , etc., with an appropriate amount calculated appropriately, in an object / hollow body (uniform or various forms) belonging to a closed system), mainly: Equilibrium of forces acting on two bodies (hollow body and fluid) in direct interaction (inappropriate* physics based on given theoretical formulas: F1+(-)F2=0, F1=(-)F2) Instead, applying force imbalance (new theoretical formulas: F1+(-)F1=0, F2+(-)F2=0, still valid physical phenomenon based on F1≠F2), the same While reciprocating and circulating various fluids (various fluid substances) in the hollow body by a predetermined method and mechanical operation, both ends of the hollow body (locally different in volume, area, etc.)・On both sides (inner surface), based on the related formula: P = F / S, relative pressure (internal pressure) that contrasts with each surface ・Differential pressure on each dynamic pressure etc. is generated not a little A pressure (internal pressure) differential (space) propulsion system and related equipment that can generate a propulsive force (forward or backward force) that can perform physical work in the (hollow) body itself. One set. (*Refer to the English text in this patent application for justifiable grounds for the display/notation of “inappropriate” in this section) In the object/hollow body belonging to the closed fluid system described in the previous section, the force imbalance (new theoretical formula: F1+(-)F1= 0 = F2 + (-) F2, F1 ≠ F2), various fluids (various fluid substances) are generated in the same hollow body (with hidden kinetic energy) at any time. When reciprocating or circulating due to the method or machine operation, especially when the fluid substance in question pushes the wall surface (inner surface) of the rear part of the same hollow body (of various shapes), not a little rearward force is generated. , The flow barrier / barrier method to reduce (if the fluid is generally gaseous, when blowing down mainly from the front in the direction of travel to the rear, crosswinds that are perpendicular to the front and back are artificially caused, and almost While adopting an air barrier method that efficiently blocks the backward force generated (derivative) on synchronization (expected) and an air & water <jet> barrier method by mixing gas and liquid) etc., the same hollow A pressure (internal pressure) differential (space) propulsion system that can effectively and continuously generate propulsive force as much as possible while creating a corresponding pressure (internal pressure) difference around both ends (both sides / inside) of the body, and A set of related equipment. When the working fluid (fluid substance) for each predetermined barrier flow path according to claim 2 is constantly circulated in the main hollow body from the rear (lower) of both sides to the front (upper) around the head In order to reduce the rearward force generated as much as possible, once the flow path for main propulsive force generation and the flow paths for various barriers are separated from the point of intersection (point of intersection), especially the fluid for the barrier While detouring through an attached bypass channel, the fluid itself does not naturally apply backward force (downward force), and is mostly sucked by the fluid machinery (including various types) near the front (upper). A set of differential pressure propulsion augmentation systems and associated equipment of single or multi-stage channel type (single or composite structure) designed to be immersed (siphoned). Regarding the (space) propulsion system according to claim 1, in particular, as a main method and technique for thrust reinforcement, a predetermined fluid (gas, etc.) using compressors (including, if necessary, push plates with small vents in some places) that can compress the mainstream fluid (mainly gas) at a correspondingly high pressure. Or, a kind of special rotating body such as a windmill or a watermill (especially, a bowl-shaped impeller etc. that can change and transform the angle of the blade blades, etc., and if necessary, a very small hole While using empty buckets and runners, etc., after compressing the pressure, steam pressure (due to the operation of a water tube boiler, etc.), water pressure (in a mixed state), hydraulic pressure, etc., Mainly toward the front (nearest inner surface) of the main body, by pushing it out continuously and strongly, while continuing to generate a high and low differential pressure between the front and rear surfaces, the pressure based on the principle of propulsion ( A set of differential pressure type propulsion reinforcement system and related equipment designed to create an internal pressure difference. Regarding the (space) propulsion system according to claim 1, etc., as a main method and technique for increasing thrust, from both sides, left and right behind the main propellant body (hollow body), especially curved routes (If necessary, it can be hung in a curved shape, etc., and arranged to reduce the centrifugal force and backward force caused by hitting the ball.) with related items added), continuously projecting to the front of the hollow body, pushing out the front surface of the same body (if essential, the inner surface with shock absorbing material etc.) , When the projectile in question reaches roughly the top, it is immediately made to make a U-turn through a predetermined turning passage, etc. From the direction), by continuing to apply an appropriate amount of magnetic force (mainly attractive force) due to the operation of an electromagnet-related accessory (attached slightly to the rear), the projectile ( While attracting an iron ball, etc.), while weakening the speed of the same projectile trying to move backward, it will be applied to the rear and reduce the backward force as much as possible, and the iron in the original place. A set of main electromagnetic differential pressure type propulsion reinforcement systems and related equipment that continuously return to the ball launcher (rear local area). In each flow path in the main hollow body according to claim 1, etc., a blade plane shape (various types) that is in contact with the main body is attached at key points, and if necessary, the flow rate (air volume ) After adding adjusting plates and rectifying plates, the pressure (external pressure) difference generated and generated lift applied to the airfoil itself is extended to the propulsive force applied to the entire main body (outside and around the blade) A set of airfoil type, pressure (internal pressure) differential propulsion system and related equipment (including flow rate, air volume controller, etc.). After laying separate flow paths with different dynamic pressures at both ends (front and back or left and right) of the hollow body according to claim 1 etc., the fluid and the main body ( Considering the angle of collision with the road surface, etc., a suitable differential pressure (for changing the course) is generated, and a direction changer that applies rotational moment, angular momentum, etc. separately in the hollow body. A set of this propulsion direction change system and related equipment consisting of a special structure attached. To the propulsion body of claim 1, etc., a propulsion force adjustment/(position) control device, etc., which can adjust the degree of thrust (in addition to the impulse), etc., is attached at an appropriate place, and the same device and the preceding paragraph are attached at any time. While making full use of direction changing devices, angle/position sensors, etc. (synchronously), in the main space sphere, while giving the body itself a certain holding power and reinforcing power, it can stay in space (space Using this propulsion device (which does not need to orbit the earth), it can replace the conventional artificial satellites that need to orbit the earth. A set of global network systems for communications, weather, etc., and a position information system and related equipment (including related electronic information and communication equipment) that serve as a lighthouse in the outer space (in the ocean of extreme space). Thrust energy that continues to be generated by the operation of various equipment for space propulsion according to claims 1 to 8 (including those whose impulse and force can be adjusted in the preceding paragraph), or the same equipment itself (provided at a predetermined position) In general, the ability to pull up (do physical work) from the weightless space outside the earth sphere, such as the following structures (one by one) While also being used as a reinforcement for , in particular, space (mainly low point, fixed point stay in space, stay in space, etc., which does not require a space tether with a height or length that exceeds that of geostationary orbit) Elevators and stratospheric (airship) platforms (connected to the main vertical orbit of the space elevator), (complex) aerospace structures derived from these ideas, etc. construction method (space construction system) and a set of related equipment.

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