High-speed impacting penetrator structure for detecting lunar soil

A penetrator and detection instrument technology, applied in the field of high-speed impact penetrator structures, can solve problems such as complex dynamics, high technical difficulty, weak gravity, etc., and achieve improved vibration reduction and protection performance, good stiffness performance, and space saving Effect

Inactive Publication Date: 2016-09-07
SHENYANG INST OF AUTOMATION - CHINESE ACAD OF SCI
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  • Abstract
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  • Claims
  • Application Information

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Problems solved by technology

Surrounding detection and lander detection are currently widely used celestial body detection methods at home and abroad, but the surrounding detection cannot detect the material in the surface of the celestial body, and the landing detection requires the lander to log in to the cel...

Method used

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  • High-speed impacting penetrator structure for detecting lunar soil
  • High-speed impacting penetrator structure for detecting lunar soil
  • High-speed impacting penetrator structure for detecting lunar soil

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Embodiment Construction

[0028] In order to make the object, technical solution and advantages of the present invention clearer, the present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments.

[0029] Such as Figure 1-4 As shown, the present invention provides a high-speed penetrator structure for lunar soil exploration, including a penetrator housing 1, a penetrator submersible head 2, a separation end cover 3, an instrument installation module 4, and a buffer damping layer 5 And the submersible head vibration damping structure 6, wherein the inner wall of the penetrator housing 1 is provided with a buffer damping layer 5, and the inside is provided with a plurality of instrument installation modules 4 for installing star detection instruments, the penetrator housing 1 The front end and the rear end of the penetrator submersible head 2 and the separation end cover 3 are connected respectively, and the submersible head vibration damping...

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Abstract

The invention relates to a high-speed impacting penetrator structure and particularly relates to a high-speed impacting penetrator structure for detecting lunar soil. The high-speed impacting penetrator structure comprises a penetrator shell, a penetrator hidden head, a separation end cover, instrument mounting modules, a buffering damping layer and a hidden head vibration-absorption damping structure, wherein the buffering damping layer is arranged on the inner wall of the penetrator shell and the penetrator shell is internally provided with the plurality of instrument mounting modules for mounting a planet detection instrument; the front end and the rear end of the penetrator shell are connected with the penetrator hidden head and the separation end cover respectively; and the penetrator hidden head is internally provided with the hidden head vibration-absorption damping structure. The high-speed impacting penetrator structure is light in weight and high in rigidity, has a good vibration-absorption performance and can be used for effectively impacting and penetrating a small celestial body, so that scientific detection on inner composition and structure of the moon is carried out.

Description

technical field [0001] The invention relates to a high-speed impact penetrator structure, in particular to a high-speed impact penetrator structure for lunar soil exploration. Background technique [0002] As a means of celestial body detection, the high-speed penetrator uses an orbiter to carry an impact penetrator to impact the celestial body at high speed so that the instrument can be embedded on the surface of the celestial body in a collision manner to detect the interior of the celestial body. Surrounding detection and lander detection are currently widely used celestial body detection methods at home and abroad, but the surrounding detection cannot detect the material in the surface of the celestial body, and the landing detection requires the lander to log in to the celestial body for direct observation, which is technically difficult and in the registration stage. The cost is huge, especially for the detection of small celestial bodies, due to its complex dynamics, ...

Claims

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Application Information

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IPC IPC(8): G01N33/24
CPCG01N33/24
Inventor 骆海涛刘广明富佳于敏于长帅王鹏
Owner SHENYANG INST OF AUTOMATION - CHINESE ACAD OF SCI
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