Star laser communication silicon-titrium sphere nuclear fusion laser emission propeller

Abstract

This invention relates to the fields of aerospace propulsion and laser communication technology, specifically to an interplanetary laser communication silicon-tritium sphere nuclear fusion laser emission thruster, comprising a silicon-tritium sphere nuclear fusion laser emitter and a laser communication device. By employing nuclear fusion technology, silicon and tritium elements are fused under high temperature and high pressure to generate energy, which is then converted into laser light and emitted, providing powerful propulsion for rockets. This solves the technical problem that existing aerospace propulsion technologies mostly use chemical rockets or ion thrusters, which have low propulsion force and long acceleration times, failing to meet the needs of future deep space exploration. By modulating and demodulating the generated laser signal, rapid data transmission can be achieved, thus solving the technical problem that existing laser communication technologies mostly use semiconductor lasers as the emission source, where the transmission distance and data rate are limited.

Description

Technical Field

[0001] This invention relates to the fields of aerospace propulsion and laser communication technology, and in particular to an interplanetary laser communication silicon-tritium sphere nuclear fusion laser emission propulsion device. Background Technology

[0002] With the development of science and technology, human exploration of space is becoming increasingly in-depth, and deep space exploration technology is also constantly developing. As deep space exploration technology continues to develop, it is expanding into deeper spaces. Among these technologies, laser communication and aerospace propulsion are key technologies for space exploration.

[0003] Most existing laser communication technologies use semiconductor lasers as the emission source. When using semiconductor lasers as the emission source, the transmission distance and data rate of the laser are limited. In addition, most existing aerospace propulsion technologies use chemical rockets or ion thrusters, but their propulsion force is small and the acceleration time is long, which cannot meet the needs of future deep space exploration.

[0004] To address the aforementioned issues, developing a laser communication and aerospace propulsion technology with longer transmission distances, higher data rates, and greater propulsion power is an urgent task. Summary of the Invention

[0005] The purpose of this invention is to provide a silicon-tritium sphere nuclear fusion laser emission thruster for interplanetary laser communication, which solves the technical problems that most existing laser communication technologies use semiconductor lasers as the emission source, which limits the transmission distance and data rate of the laser. It also addresses the technical problems that most existing aerospace propulsion technologies use chemical rockets or ion thrusters, which have low propulsion force and long acceleration time, and cannot meet the needs of future deep space exploration.

[0006] To achieve the above objectives, this invention provides an interplanetary laser communication silicon-tritium sphere nuclear fusion laser emission propulsion device, comprising a silicon-tritium sphere nuclear fusion laser emitter and a laser communication device. The silicon-tritium sphere nuclear fusion laser emitter uses nuclear fusion technology to generate energy and converts the generated energy into laser signals for emission, providing powerful propulsion for the rocket. The laser communication device generates a laser beam, processes it, and then emits the laser beam. It then receives and processes the emitted laser beam and displays the resulting image, thus achieving data transmission.

[0007] The silicon-tritium sphere nuclear fusion laser emitter fuses silicon and tritium elements under high temperature and high pressure, and uses nuclear fusion technology to generate the required energy.

[0008] The laser communication device includes a laser transmitter and a laser receiver. The laser transmitter is used to modulate and demodulate the generated laser beam and then emit the modulated and demodulated laser beam. The laser receiver is used to receive the laser beam emitted by the laser transmitter and perform image processing on the received laser beam to obtain image data.

[0009] The laser transmitter includes a laser, an optical modulator, and an optical transmitting antenna. The laser is used to generate a laser beam for communication and transmit the generated laser beam to the optical modulator connected to the laser. The optical modulator is used to modulate and demodulate the laser beam. The optical transmitting antenna is used to transmit the modulated and demodulated laser beam.

[0010] The laser receiver includes an optical receiving antenna, a photodetector, and an imager. The optical receiving antenna receives the emitted laser beam and transmits it to the photodetector. The photodetector converts the received laser beam into an electrical signal and processes the converted electrical signal. The imager converts the processed electrical signal into image data.

[0011] The laser communication device further includes an image processor and a display screen. The image processor processes the image data converted by the imager and transmits the processed image data to the display screen. The display screen displays the image processed by the image processor.

[0012] The laser communication device employs multiplexing technology to transmit multiple data streams simultaneously.

[0013] This invention discloses a silicon-tritium sphere nuclear fusion laser emission thruster for interstellar laser communication. By employing nuclear fusion technology, silicon and tritium are fused under high temperature and pressure to generate energy, which is then converted into laser light and emitted. This provides powerful propulsion for rockets, thus solving the technical problem that most existing aerospace propulsion technologies use chemical rockets or ion thrusters, which have low thrust and long acceleration times, failing to meet the needs of future deep space exploration. By modulating and demodulating the generated laser signal, rapid data transmission can be achieved, thereby addressing the technical problem that most existing laser communication technologies use semiconductor lasers as the emission source, where the transmission distance and data rate are limited. Attached Figure Description

[0014] To more clearly illustrate the technical solutions in the embodiments of this application or the prior art, the accompanying drawings used in the description of the embodiments or the prior art will be briefly introduced below.

[0015] Figure 1 This is a control principle diagram of the laser communication device of the interstellar laser communication silicon-tritium sphere nuclear fusion laser emission thruster according to the first embodiment of the present invention.

[0016] In the diagram: 101-Laser transmitter, 102-Laser receiver, 103-Image processor, 104-Display screen, 105-Laser, 106-Optical modulator, 107-Optical transmitting antenna, 108-Optical receiving antenna, 109-Photodetector, 110-Imager. Detailed Implementation

[0018] The embodiments of the present invention are described in detail below. Examples of the embodiments are shown in the accompanying drawings. The embodiments described below with reference to the accompanying drawings are exemplary and intended to explain the present invention, but should not be construed as limiting the present invention.

[0019] First embodiment: Please see Figure 1 , Figure 1 This is a control principle diagram of the interstellar laser communication silicon-tritium sphere nuclear fusion laser emission thruster according to the first embodiment of the present invention. The present invention provides an interstellar laser communication silicon-tritium sphere nuclear fusion laser emission thruster, including a silicon-tritium sphere nuclear fusion laser emitter and a laser communication device. The laser communication device includes a laser emitter 101, a laser receiver 102, an image processor 103, and a display screen 104. The laser emitter 101 includes a laser 105, an optical modulator 106, and an optical transmitting antenna 107. The laser receiver 102 includes an optical receiving antenna 108, a photodetector 109, and an imager 110.

[0020] In this embodiment, the present invention utilizes nuclear fusion technology to fuse silicon and tritium elements under high temperature and high pressure to generate energy, which is then converted into laser light and emitted, providing powerful propulsion for rockets. This addresses the technical problem that existing aerospace propulsion technologies, which mostly use chemical rockets or ion thrusters, suffer from low propulsion force and long acceleration time, failing to meet the needs of future deep space exploration. By modulating and demodulating the generated laser signal, rapid data transmission can be achieved, thus solving the technical problem that existing laser communication technologies, which mostly use semiconductor lasers as the emission source, have limited transmission distance and data rate.

[0021] The silicon-tritium sphere nuclear fusion laser emitter uses nuclear fusion technology to generate energy and converts the generated energy into laser signals for emission, providing powerful propulsion for the rocket. The laser communication device generates a laser beam, processes it, and then emits the laser beam. It then receives and processes the emitted laser beam and displays the resulting image, thus achieving data transmission.

[0022] Secondly, the silicon-tritium sphere nuclear fusion laser emitter fuses silicon and tritium elements under high temperature and high pressure environment, and uses nuclear fusion technology to generate the required energy.

[0023] Furthermore, the laser emitter 101 is used to modulate and demodulate the generated laser beam and then emit the modulated and demodulated laser beam; the laser receiver 102 is used to receive the laser beam emitted by the laser emitter 101 and perform image processing on the received laser beam to obtain image data.

[0024] Meanwhile, the laser 105 is used to generate a communication laser beam and transmit the generated laser beam to the optical modulator 106 connected to the laser 105; the optical modulator 106 is used to modulate and demodulate the laser beam; the optical transmitting antenna 107 is used to transmit the modulated and demodulated laser beam, and the laser 105 is a deep space laser diode.

[0025] In addition, the optical receiving antenna 108 is used to receive the emitted laser beam and transmit it to the photodetector 109; the photodetector 109 is used to convert the received laser beam into an electrical signal and process the converted electrical signal; the imager 110 is used to convert the processed electrical signal into image data, and the photodetector 109 is an avalanche diode (APD).

[0026] Finally, the image processor 103 processes the image data converted by the imager 110 and transmits the processed image data to the display screen 104; the display screen 104 displays the image processed by the image processor 103. The laser communication device uses multiplexing technology to transmit multiple data streams simultaneously.

[0027] When using the interplanetary laser communication silicon-tritium sphere nuclear fusion laser emission thruster of this embodiment, in terms of the propulsion system, the silicon-tritium sphere nuclear fusion laser emitter employs nuclear fusion technology, fusing silicon and tritium elements under high temperature and high pressure to generate energy, which is then converted into laser light and emitted. Because the silicon-tritium sphere nuclear fusion laser emitter has extremely high energy density and power, it can provide strong propulsion for rockets. Furthermore, due to the use of nuclear fusion technology and the abundant energy sources of silicon and tritium elements used in the silicon-tritium sphere nuclear fusion laser emitter, it can meet the needs of long-term space exploration. In terms of laser communication, the laser 105 generates a communication laser beam, which is then transmitted to the optical modulator 106 connected to the laser 105. The laser beam is modulated and demodulated in the optical modulator 106, and then emitted through the optical transmitting antenna 107. When the laser beam is emitted, it is received by the optical receiving antenna 108 and transmitted to the photodetector 109. The photodetector 109 then converts the received laser beam into an electrical signal, processes the signal, and converts it into image data. Finally, the image processor 103 processes the image data converted by the imager 110 and transmits the processed image data to the display screen 104, which displays the image processed by the image processor 103. This achieves data transmission and completes laser communication between the rocket and the ground. Because lasers have high frequencies and narrow beams, long-distance, high-speed communication is possible, reaching speeds of 16 million kilometers per second. Furthermore, the laser 105 is a deep-space laser diode, and the modulation and reception technology employs direct intensity modulation and direct intensity detection (MID). The laser communication device uses a method of direct conversion of the transmitted laser via OOK data stream (DD), with an avalanche diode-like detector (APD). In addition, the laser communication device uses multiplexing technology to transmit multiple data streams simultaneously, further improving the co-current efficiency.

[0028] The interstellar laser communication silicon-tritium sphere nuclear fusion laser emission thruster described above has the following advantages: 1. High bandwidth: Laser communication can provide high bandwidth and transmit large amounts of data, thus having an advantage in situations where a large amount of data transmission is required.

[0029] 2. Low energy consumption: Compared with traditional electromagnetic wave communication, laser communication systems consume less energy, which helps to reduce energy consumption and costs.

[0030] 3. Low interference: Laser communication technology communicates in the optical band, avoiding electromagnetic interference, resulting in more stable and reliable signal quality.

[0031] In summary, this invention utilizes nuclear fusion technology to fuse silicon and tritium elements under high temperature and pressure to generate energy, which is then converted into laser light and emitted, providing powerful propulsion for rockets. This addresses the technical problem that existing aerospace propulsion technologies, which mostly employ chemical rockets or ion thrusters, suffer from low propulsion force and long acceleration times, failing to meet the demands of future deep space exploration. By modulating and demodulating the generated laser signal, rapid data transmission can be achieved, thus solving the technical problem that existing laser communication technologies, which mostly use semiconductor lasers as the emission source, are limited in terms of transmission distance and data rate.

[0032] The above-disclosed embodiments are merely one or more preferred embodiments of this application and should not be construed as limiting the scope of this application. Those skilled in the art can understand that all or part of the processes for implementing the above embodiments and equivalent changes made in accordance with the claims of this application still fall within the scope of this application.

Claims

1. A silicon-tritium sphere nuclear fusion laser emission propulsion device for interstellar laser communication, characterized in that, The system includes a silicon-tritium sphere nuclear fusion laser emitter and a laser communication device. The silicon-tritium sphere nuclear fusion laser emitter uses nuclear fusion technology to generate energy and converts the generated energy into laser signals for emission, providing powerful propulsion for rockets. The laser communication device generates a laser beam, processes it, and then emits the laser beam. It then receives and processes the emitted laser beam and displays the resulting image, thus achieving data transmission.

2. The interstellar laser communication silicon-tritium sphere nuclear fusion laser emission thruster as described in claim 1, characterized in that, The silicon-tritium sphere nuclear fusion laser emitter fuses silicon and tritium elements under high temperature and high pressure, and uses nuclear fusion technology to generate the required energy.

3. The interstellar laser communication silicon-tritium sphere nuclear fusion laser emission thruster as described in claim 1, characterized in that, The laser communication device includes a laser transmitter and a laser receiver. The laser transmitter is used to modulate and demodulate the generated laser beam and then emit the modulated and demodulated laser beam. The laser receiver is used to receive the laser beam emitted by the laser transmitter and perform image processing on the received laser beam to obtain image data.

4. The interstellar laser communication silicon-tritium sphere nuclear fusion laser emission thruster as described in claim 3, characterized in that, The laser transmitter includes a laser, an optical modulator, and an optical transmitting antenna. The laser is used to generate a laser beam for communication and transmits the generated laser beam to the optical modulator connected to the laser. The optical modulator is used to modulate and demodulate the laser beam. The optical transmitting antenna is used to transmit the modulated and demodulated laser beam.

5. The interstellar laser communication silicon-tritium sphere nuclear fusion laser emission thruster as described in claim 4, characterized in that, The laser receiver includes an optical receiving antenna, a photodetector, and an imager. The optical receiving antenna is used to receive the emitted laser beam and transmit it to the photodetector. The photodetector is used to convert the received laser beam into an electrical signal and process the converted electrical signal. The imager is used to convert the processed electrical signals into image data.

6. The interstellar laser communication silicon-tritium sphere nuclear fusion laser emission thruster as described in claim 5, characterized in that, The laser communication device further includes an image processor and a display screen. The image processor is used to process the image data converted by the imager and transmit the processed image data to the display screen; the display screen is used to display the image processed by the image processor.

7. The interstellar laser communication silicon-tritium sphere nuclear fusion laser emission thruster as described in claim 1, characterized in that, The laser communication device employs multiplexing technology to transmit multiple data streams simultaneously.

Images