Manned lunar surface electromagnetic emission lunar surface acceleration orbit

An electromagnetic and orbital technology, applied in the field of deep space exploration, can solve the problems of the scale of the launch device and the large peak electromagnetic power, and achieve the effect of saving propellant and reducing the risk of overturning

Active Publication Date: 2019-04-05
BEIJING SPACE TECH RES & TEST CENT
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

At the same time, some research has begun to involve electromagnetic launch vehicle, but the scale of the launch device and the peak electromagnetic power are very large, and it is still in the key technology research stage

Method used

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  • Manned lunar surface electromagnetic emission lunar surface acceleration orbit
  • Manned lunar surface electromagnetic emission lunar surface acceleration orbit
  • Manned lunar surface electromagnetic emission lunar surface acceleration orbit

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Embodiment Construction

[0025] In order to more clearly describe the embodiments of the present invention or the technical solutions in the prior art, the following will briefly introduce the drawings that are used in the embodiments. Apparently, the drawings in the following description are only some embodiments of the present invention, and those skilled in the art can also obtain other drawings according to these drawings without creative efforts.

[0026] When describing the embodiments of the present invention, the terms "vertical", "transverse", "upper", "lower", "front", "rear", "left", "right", "vertical", " The orientation or positional relationship expressed by "horizontal", "top", "bottom", "inner" and "outer" is based on the orientation or positional relationship shown in the relevant drawings, which are only for the convenience of describing the present invention and simplifying the description, and It is not to indicate or imply that the device or element referred to must have a particu...

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Abstract

The invention relates to a manned lunar surface electromagnetic emission lunar surface acceleration orbit. The orbit is characterized in that the orbit comprises an entrance section, an annular acceleration section and exit sections, wherein a lunar surface ascender exits out of a base station and enters a transitional section of an electromagnetic emission entrance, one electromagnetic emission device is only provided with one entrance section, and the length is at 100-m order of magnitude; in the main working stage of electromagnetic emission, the electromagnetic emission device gradually increases the speed of the lunar surface ascender relative to the lunar surface to an exit state required value from zero through multiple circles of boosting, only one annular acceleration section is designed for one electromagnetic emission device, and the radius is at 2-km order of magnitude; and the lunar surface ascender is led out from the annular acceleration section, the height is increased,the direction is adjusted, smooth transition to the annular acceleration section and a following powered flight stage is ensured, and the four exit sections are designed for one electromagnetic emission device. A certain initial motion state is established for the lunar surface ascender in an electromagnetic emission mode in the manned lunar surface take-off ascending process, the velocity increment can be shared, and plenty of a propellant can be saved.

Description

technical field [0001] The invention belongs to the technical field of deep space exploration, in particular to a manned lunar surface electromagnetic launch lunar surface acceleration track. Background technique [0002] With the advancement of lunar exploration missions, it will gradually become possible to establish a lunar base suitable for long-term human presence on the moon in the future. With the support of the lunar base, comprehensive and systematic exploration of the moon and large-scale resource development and utilization can be carried out. [0003] The round-trip transportation between the Earth and the Moon can be divided into three parts: the Earth side (ground launch and re-entry return), the Earth-Moon (Earth-Moon transfer and Moon-ground transfer), and the Moon side. There are two stages of take-off and ascent on the lunar surface, and the total speed increment is about 4000m / s. [0004] The traditional lunar surface take-off and ascent adopts chemical p...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G1/24B64G1/22B64G1/12
CPCB64G1/12B64G1/22B64G1/24
Inventor 田林王平彭坤侯振东孙兴亮苏怀朋
Owner BEIJING SPACE TECH RES & TEST CENT
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