Langmuir probe sensor used on sounding rocket

A technology of Langmuir probes and sounding rockets, applied in the field of space detection, can solve the problems of mutual constraints between shielding effect and vibration magnitude, and achieve the effect of enhancing stiffness

Inactive Publication Date: 2015-06-03
NAT SPACE SCI CENT CAS
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  • Abstract
  • Description
  • Claims
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Problems solved by technology

[0005] The purpose of the present invention is to provide a Langmuir probe used for sounding rockets in order to solve the technical problem of mutual restriction between the shielding effect and the vibration level caused by the existing Langmuir probe sensor due to its own structure. Sensor; the Langmuir probe sensor can not only meet the vibration level requirements, but also ensure a good shielding effect on the extension rod and the arrow body

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  • Langmuir probe sensor used on sounding rocket
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  • Langmuir probe sensor used on sounding rocket

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Embodiment Construction

[0021] The Langmuir probe sensor used on the sounding rocket according to the present invention will be described in detail below with reference to the drawings and embodiments.

[0022] Such as figure 2 As shown, a Langmuir probe sensor used on a sounding rocket according to the present invention, the Langmuir probe sensor includes: upper hemisphere 1, lower hemisphere 2, connecting rod 4, extension rod (not shown) and signal lines (not shown), the upper hemisphere 1, the lower hemisphere 2 and the connecting rod 4 are all hollow structures, the upper hemisphere 1 and the lower hemisphere 2 are connected by an insulating partition 3, and the connecting rod One end of 4 penetrates along the central axis of the spherical side of the lower hemisphere 2, and the connecting rod 4 is connected and fixed with the lower hemisphere 2 through the insulating pad 6 nested on one end of the connecting rod 4, and the other end is connected and fixed with the extension rod One end of the ...

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Abstract

The invention provides a Langmuir probe sensor used on a sounding rocket. The Langmuir probe sensor comprises an upper hemisphere (1), a lower hemisphere (2), a connecting rod (4), a telescopic rod and a signal wire, wherein the upper hemisphere (1), the lower hemisphere (2) and the connecting rod (4) are in cavity structures; the upper hemisphere (1) and the lower hemisphere (2) are connected through an insulating partition plate (3); one end of the connecting rod (4) penetrates in along a central shaft at one side of the spherical surface of the lower hemisphere (2); the connecting rod (4) and the lower hemisphere (2) are connected and fixed through an insulating pad (6) embedded in one end of the connecting rod (4), the other end of the connecting rod (4) is connected and fixed together with the telescopic rod; one end of the signal wire is connected with the upper hemisphere (1), the other end of the signal wire (1) penetrates through the insulating pad (6) and the inner cavity of the upper hemisphere (1), and is guided out from the inner cavity of the connecting rod (4); the upper hemisphere (1) is used as a collecting electrode, and the lower hemisphere (2) is used as a protective pole.

Description

technical field [0001] The invention relates to the technical field of space detection, in particular to a Langmuir probe sensor used on a sounding rocket. Background technique [0002] Langmuir probe sensor is an important instrument for in-situ measurement of space plasma electron density and electron temperature. It is widely used in ionospheric satellite and rocket detection. Before this mission, there is no successful application precedent in our country. Langmuir probe sensor technology is one of its key technologies and one of the key factors to determine the success of detection. [0003] Currently, the Langmuir probe sensor consists of three parts: collector, guard and extension rod. The collector (usually loaded with scanning voltage or fixed bias) interacts with the surrounding plasma to collect charged particles in the space to form a collection current, which is measured by the measured circuit to form a signal output; the protection electrode maintains the sam...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01N27/00
Inventor 关燚炳刘超张爱兵孔令高朱光武孙越强梁金宝丁建京郑香脂田峥安雅雅董永进林强孟强强
Owner NAT SPACE SCI CENT CAS
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