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Mars floating detection system

A detection system and floating technology, applied in the field of aircraft to achieve the effect of wide detection range

Active Publication Date: 2020-09-01
CENT SOUTH UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The current detection of the Martian environment mainly relies on Mars orbiters and rovers, and it is impossible to achieve detailed detection of the low-altitude and middle-altitude atmospheric environment of Mars

Method used

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  • Mars floating detection system

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Embodiment Construction

[0028] Such as figure 1 As shown, the Mars floating detection system disclosed in this embodiment includes a floating system 1, an inflation system 2 and a landing cabin 3; the floating system 1 and the inflation system 2 are both placed in the landing cabin 3.

[0029] Such as figure 2 As shown, the floating system 1 includes an overpressure balloon 11 , a tether 12 , an instrument cabin 13 and a trajectory controller 14 . The instrument cabin 13 is tied under the superpressure balloon by a tether 12, and the trajectory controller 14 is tied under the instrument cabin by a tether.

[0030] The super-pressure balloon 11 adopts a pumpkin-shaped super-pressure balloon, the inflatable medium is helium, and the airbag is strong enough to withstand the pressure difference caused by superheat and super-cold phenomena, so as to maintain a stable flight altitude. At the same time, a flexible thin-film solar cell is installed on the top of the super-pressure balloon 15. Store the ge...

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Abstract

The invention discloses a Mars floating detection system. The system comprises a floating system, an inflation system and a landing cabin, wherein the floating system comprises an overpressure balloon, a tying rope, an instrument cabin and a track controller, the track controller comprises a main rod, a main wing, an empennage and a balance weight, the main wing is connected to the middle of the main rod, the empennage and the balance weight are arranged at the two ends of the main rod respectively, the instrument cabin is tied below the overpressure balloon through the tying rope, and the track controller is tied below the instrument cabin; the inflation system is arranged in the landing cabin and used for inflating the overpressure balloon. The system is carried by a lander to reach thesurface of the Mars, and when the meteorological condition of the surface of the Mars is good, the inflation system inflates the overpressure balloon until the floating system lifts off and is separated from the landing cabin; then the floating system is separated from the inflation system, and the inflation system is left in the landing cabin; and after the floating system reaches a preset height, detection work is started, and different areas are detected through Mars atmospheric motion. Movement is not limited by Mars topography and geomorphism, and the detection range is wider.

Description

technical field [0001] The invention belongs to the technical field of aircraft, in particular to a Mars floating detection system. Background technique [0002] With the rapid development of the space industry of various countries in the world, Mars exploration technology has been further improved. The current detection of the Martian environment mainly relies on Mars orbiters and rovers, which cannot achieve detailed detection of the low-altitude and middle-altitude atmospheric environment of Mars. Contents of the invention [0003] The purpose of the present invention is to provide a Mars floating detection system capable of detecting the Martian mid-low altitude atmospheric environment and the Martian surface, aiming at the deficiencies of the prior art. [0004] This Mars floating detection system provided by the present invention comprises a floating system, an inflation system and a landing cabin; Empennage and weighing hammer, the main wing is connected to the mi...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G1/10B64G1/22B64G1/62B64G1/64B64G1/66
CPCB64G1/10B64G1/22B64G1/62B64G1/645B64G1/66
Inventor 罗世彬李珺廖俊冯彦斌杨泽川袁俊杰
Owner CENT SOUTH UNIV
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