Mars exploration method and Mars probe

A technology of Mars probe and detection method, which is applied in the aerospace field and can solve problems such as high cost

Active Publication Date: 2018-05-04
SHANGHAI AEROSPACE SYST ENG INST
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  • Abstract
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  • Claims
  • Application Information

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Problems solved by technology

However, the existing methods of Mars exploration have the problem of high cost when conducting Mars exploration

Method used

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  • Mars exploration method and Mars probe
  • Mars exploration method and Mars probe
  • Mars exploration method and Mars probe

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Embodiment Construction

[0038] In order to solve the above-mentioned problems in the prior art, the technical solution adopted in the embodiment of the present invention is to use only one Mars probe to enter the atmosphere of Mars when sampling Mars, and the Mars probe uses atmospheric braking to complete Mars capture, and Instead of using its own fuel for braking, the fuel consumption of the probe can be saved, so the cost of Mars exploration can be effectively saved.

[0039] In order to make the above objects, features and advantages of the present invention more comprehensible, specific embodiments of the present invention will be described in detail below in conjunction with the accompanying drawings.

[0040] figure 1 A flow chart showing a Mars detection method in an embodiment of the present invention; figure 2 It is a schematic diagram of the position of the Mars probe in the embodiment of the present invention when it conducts Mars exploration. to combine figure 2 ,Such as figure 1 T...

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Abstract

The embodiment of the invention provides a Mars exploration method and a Mars probe. The Mars exploration method comprises the steps that the Mars probe is launched from the earth, lifts off and enters an earth Mars transfer orbit, orbit trimming is conducted, and the Mars probe enters a Mars atmospheric layer; pneumatic braking is conducted through the Mars atmospheric layer, and the Mars probe enters and parks on a large elliptical orbit around the Mars; when the Mars probe parks on the large elliptical orbit around the Mars, dust storm on the Mars is monitored; and when the situation that the dust storm on the Mars is formed is determined, the Mars probe enters the Mars atmospheric layer to sample the dust storm on the Mars. According to the scheme, the cost can be reduced during Mars exploration.

Description

technical field [0001] The invention relates to the field of aerospace technology, in particular to a Mars detection method and a Mars probe. Background technique [0002] Martian dust is tiny particles formed by the evolution of Martian surface soil over hundreds of millions of years. It is carried into the air by factors such as Martian atmospheric circulation and the static environment on the Martian surface, forming Martian dust storms, a unique Martian meteorological and astronomical phenomenon. [0003] According to the current scientific detection results, Mars can form a large-area Martian dust storm around the surface of Mars. Among them, the main factor for the outbreak of Martian dust storm is that the Martian atmosphere brings tiny particles of Martian dust into the air. After the dust absorbs sunlight in the air, the temperature of the atmosphere rises, which further intensifies the movement of the Martian atmosphere and further accelerates the development of th...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G1/10B64G1/66
CPCB64G1/105B64G1/66B64G1/1064
Inventor 袁勇陈辉禹志赵晨梅海李志刚胡震宇
Owner SHANGHAI AEROSPACE SYST ENG INST
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