Lunar surface pneumatic power generation method based on secondary utilization of propulsion residual resources

Abstract

The invention relates to a lunar surface pneumatic power generation method based on secondary utilization of propulsion residual resources. The method includes the steps that a, a double-component extrusion type propulsion system is adopted for carrying a large amount of high-pressure gas and propellants for providing flying power for a lunar surface landing detector; b, after the lunar surface landing detector lands on a lunar surface, residual propulsion resources are secondarily used for conducting pneumatic power generation; and c, a pneumatic power generation device is adopted, high-pressure gas or fuel is adopted as the input, energy in the gas pressure reduction process is used for driving a turbine to rotate, a generator rotor is driven to rotate, and a magnetic field of the generator rotor interacted with a magnetic field of a generator stator, and electric energy is output. The lunar surface pneumatic power generation method based on secondary utilization of propulsion residual resources is suitable for deep space exploration aircrafts with the large propulsion system scale and the large demand for energy in the lunar surface exploration period.

Description

technical field [0001] The present invention relates to the general technical field of space vehicles, and in particular to a lunar surface aerodynamic power generation method based on the secondary utilization of propulsion surplus resources. Background technique [0002] After landing on the lunar surface, the deep space exploration aircraft needs to deal with the harsh lunar environment, including extremely low vacuum, extreme high and low temperature, alternation of moon night and day, space radiation, moon dust, etc.; A large energy supply is required. After my country's CE-3 and CE-4 unmanned probes landed on the lunar surface, isotope heat sources were used to insulate key equipment during the moon night; the "Curiosity" unmanned Mars rover that landed on Mars in the United States in 2012 used nuclear power to move the entire vehicle. , communications, computing and thermal control to provide power. For a manned lunar lander or a sealed pressurized manned lunar vehic...

AI Technical Summary

Problems solved by technology

For the safety of lunar surface activities, the propulsion system will be passivated at an appropriate time, that is, the high-pressure gas and the remaining propellant are directly discharged into the vacuum of the lunar surface, and the energy of the high-pressure gas accumulated in the early stage is directly wasted.

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