Aerospace systems and equipment for peace and security

Abstract

The objective is to capture and store malfunctioning spacecraft, aircraft, missiles, giant meteorites, and other anomalous objects in the space sphere, and to safely return them to base, thereby preventing these objects from falling to Earth and causing disasters. [Solution] A space aerospace system and apparatus characterized in that a transport aircraft 21 carrying a space shuttle 11 first flies in the direction of an anomaly, changes direction at a predetermined location and time, matches the speed in the same direction as the anomaly, and releases the flexible arms that were fixing the space shuttle, at the same time the space shuttle ignites its engines and takes off towards a predetermined position, speed, and time, at the same time the transport aircraft retracts its flexible arms and returns to base, while the space shuttle approaches the anomaly at the predetermined location, speed, and time, extends its flexible arms to capture and retract it, and returns to base.

Description

Technical Field

[0001] The present invention is a system for ensuring safety and peace in the fields of aviation and space. Since the invention of the airplane, a century has passed. Due to various reasons, tragic accidents have occurred and precious human lives have been lost. In the future, as human travel in space becomes more popular, it is necessary to be prepared not only for various accidents in space but also for natural and man-made threats such as large meteorites and missiles.

Background Art

[0002] Technologies for constantly monitoring the vast universe and aviation circle from the ground by radar and from satellites by optical and radio wave observations are already highly developed. The safety of air travel is maintained by air traffic control. Regarding missiles, a system for quickly detecting their launches and monitoring their trajectories has already been established.

Prior Art Documents

Patent Documents

[0003]

Patent Document 1

Patent Document 2

Non-Patent Documents

[0004]

Non-Patent Document 1

Non-Patent Document 2

Summary of the Invention

Problems to be Solved by the Invention

[0005] However, there appears to be no system in place to actually fly to the site of an accident-damaged aircraft or space rocket, match its relative speed and position, capture the aircraft, and perform rescue operations. Similarly, while there are missile interception systems, there is no system to capture them and take appropriate action. The same applies to giant meteorites; their potential danger is enormous, and we must be prepared at all times. [Means for solving the problem]

[0006] The system of this invention is activated when it detects a spacecraft or aircraft that has become unable to operate normally due to an accident in space or the airspace, or an abnormal flying object such as a missile or a giant meteorite.

[0007] The system of the present invention consists of a space shuttle that flies into space to capture a target object, performs predetermined procedures on it, and then returns to the base, and a transport aircraft that carries the space shuttle to a predetermined location and gives it an initial velocity in a predetermined direction.

[0008] Figure 1 shows a space shuttle. Unlike conventional space rockets, it has a flat bottom structure. Figure 2 shows the space shuttle with its flexible arms, which are normally stored inside the vehicle, extended outwards. The flexible arms can be freely extended and bent through multiple joints. Multiple pairs of these flexible arms are provided along the vehicle's body, and they are extended to capture target objects.

[0009] Figure 3 shows the transport aircraft used in the present invention. Unlike ordinary aircraft, it is characterized by its flat upper surface. Accordingly, while conventional airplanes have a tall tail with vertical stabilizers and rudders, in the present invention, in order to achieve a flat upper surface of the fuselage, only rudders are provided, and vertical stabilizers are located on both wings. Figure 4 shows the transport aircraft carrying a space shuttle on top and securing it with flexible arms. Multiple pairs of flexible arms are provided along the fuselage on the upper part of the transport aircraft. In addition, if it is necessary to capture an object below, multiple pairs of flexible arms are also stored on the lower part of the transport aircraft.

[0010] Figure 5 illustrates the operation of the system of the present invention. Here, the position, velocity, and time of the object in space are indicated by (r, v, t). First, the spacetime at which the anomalous object is detected and the system is activated is (r0, v0, t0). Here, v0 = 0. At time t0, a transport aircraft carrying the space shuttle takes off and flies towards the target object. Just before the scheduled time (r1, v1, t1), the transport aircraft turns and changes direction. This is to make it velocate in the same direction as the target object. Subsequently, the transport aircraft releases the flexible arms that were securing the space shuttle, and at the same time, the space shuttle ignites its engines and takes off. The transport aircraft retracts its flexible arms and returns to base.

[0011] Upon arriving at the planned capture time (Ra, va, ta) of the target object, the space shuttle will detect the object using a radio reader and optical cameras, approach it, and capture it. After processing the captured object according to the system's instructions, it will return to the base.

[0012] The types of actions taken include transporting damaged spacecraft and aircraft to designated airports for soft landings, and transporting missiles and large meteorites to designated locations far from human settlements. [Effects of the Invention]

[0013] The system of this invention will ensure the safety of the space sphere and world peace. [Brief explanation of the drawing]

[0014] [Figure 1] This invention illustrates the space shuttle. [Figure 2] This shows the space shuttle with its arms extended. [Figure 3] This invention illustrates the transport aircraft of the present invention. [Figure 4] This diagram shows the transport aircraft of the present invention carrying a space shuttle. [Figure 5] This demonstrates the operation of the aerospace system of the present invention. [Modes for carrying out the invention]

[0015] The present invention will first be utilized not only for peace and security but also for ordinary space travel by spacecraft. Conventional space travel has mostly been by multi-stage rockets. Due to the fall of the first-stage rocket, the launch direction was severely restricted, and it was difficult to reuse the first-stage rocket. In the present invention, after launching the space shuttle, the carrier aircraft retracts its manipulator arm and returns to the base on its own. Also, after fulfilling its mission, the space shuttle returns to the base. Conventional space rockets do not have wings, so due to the increased speed during the fall, they become hot due to friction with the air, making it difficult to return to Earth. The space shuttle of the present invention generates lift at locations with air by means of its wings to offset gravity, slow down the fall, and safely return to Earth.

Industrial Applicability

[0016] The present invention ensures the safety of the space and aviation circles, and its industrial applicability in areas such as international and domestic travel in the space and aviation circles, defense, and prevention of natural disasters is enormous.

Explanation of Signs

[0017] 11 is the fuselage of the space shuttle of the present invention. 12 are the wings of the space shuttle. There is a pair on the left and right. 13 is the tail fin of the space shuttle. 14 is the engine of the space shuttle. 15 is the manipulator arm in front of the space shuttle. There are multiple pairs on the left and right. 15a, 15b 16 is the manipulator arm behind the space shuttle. There are multiple pairs on the left and right. 16a, 16b 21 is the fuselage of the carrier aircraft of the present invention. 22 is the tail fin of the carrier aircraft. 23 are the main wings of the carrier aircraft. There is a pair on the left and right. 24 are the vertical stabilizers of the carrier aircraft. There is a pair on the left and right. 25 are the engines of the carrier aircraft. There is a pair or multiple pairs on the left and right. 26 is the auxiliary wing of the carrier aircraft. 27. These are the movable arms of a transport aircraft. There are multiple pairs, one on each side.

Claims

1. In a space aerospace system and apparatus, which is activated upon being ordered to capture anomalous objects such as malfunctioning spacecraft, aircraft, missiles, or giant meteorites in the space aerosphere, a transport aircraft carrying a space shuttle first flies in the direction of the anomalous object, changes direction at a predetermined location and time to match the speed of the anomalous object and releases the flexible arms that were fixing the space shuttle, simultaneously ignites the engines of the space shuttle and takes off towards a predetermined position, speed, and time, and at the same time the transport aircraft retracts its flexible arms and returns to base, while the space shuttle approaches the anomalous object at the predetermined position, speed, and time, extends its flexible arms to capture it, performs predetermined procedures to separate it, retracts its flexible arms and returns to base.

2. The aforementioned space shuttle has a structure comprising a flat-bottomed body and wings, and has multiple pairs of flexible arms along the body, each equipped with a joint mechanism that is normally stored in the body and extends outward and bends freely during the object capture operation.

3. The transport aircraft has a flat top surface, and has multiple pairs of flexible arms, normally housed inside the aircraft, that extend outwards and bend freely when an object such as a space shuttle is loaded onto the top surface and secure it.

4. In order to achieve the flat upper surface, the aforementioned transport aircraft shall have vertical stabilizers above the main wings, and the tail fins, which perform the function of rudders, shall be positioned at a height that does not exceed the upper surface.

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