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Venus probe configuration

A detector and configuration technology, which is applied in the direction of artificial satellites, space vehicle power supply systems, etc., can solve the problem that the detector configuration cannot meet the needs of Venus detection, and achieves a small lateral envelope size, a low longitudinal center of mass, and a high response rate. small effect

Active Publication Date: 2012-10-10
SHANGHAI SATELLITE ENG INST
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Problems solved by technology

[0003] The purpose of the present invention is to improve a Venus detector configuration to solve the technical problem in the prior art that the detector configuration cannot meet the needs of Venus detection

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  • Venus probe configuration

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Embodiment Construction

[0017] The present invention will be described in detail below in conjunction with the accompanying drawings.

[0018] see Figure 1 to Figure 3 , a Venus probe configuration, including: an upper cabin, a lower truss structure, a radar 1, an atmospheric floater 3, a solar wing 5, four large-capacity storage tanks 6 and a large-diameter high-gain antenna 9.

[0019] The upper compartment further comprises a top plate 2, four side plates 4 and a middle composite plate 8, each side plate 4 is connected to each other, the top plate 2 is connected to the top of each side plate 4, and the middle composite plate 8 is arranged in each side plate 4 and connected with the top plate 1 connect.

[0020] The lower truss structure includes truss partitions 7, arrow connecting rings 10 and some carbon fiber rods 11, and the truss partitions 7 are connected to the bottom of each side plate 4, such as image 3 As shown, it further includes: a honeycomb sandwich panel 71, four built-in flange...

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Abstract

The invention relates to a Venus probe configuration which comprises an upper cabin and a lower truss structure. The upper cabin further comprises a top plate, a plurality of side plates and middle composition boards; the side plates are interconnected; the top plate is connected to the top part of each side plate; the middle composition boards are respectively arranged inside each side plate and are connected with the top plate; the lower truss structure comprises a truss separator; and the truss separator is connected to the bottom of each side plate. According to the invention, the installing and using requirements of parts such as an atmosphere levitron, a synthetic aperture radar, high-capacity storage boxes and the like can be met; and the Venus probe configuration is suitable for the research requirement on the Venus detection in the future and has the advantages of small transverse enveloping size and large bearing capacity. Moreover, the truss structure adopts a combination structure, the expansibility is strong, a graphite shaft is also adopted and the system thermal stability is high. Moreover, the Venus probe configuration also has the advantages of low longitudinal mass center, small response, small change of the rotational inertia, easiness for control and the like.

Description

technical field [0001] The invention relates to a probe configuration, in particular to a Venus probe configuration. Background technique [0002] my country's future Venus probes will need to carry components such as small atmospheric floaters, large-size synthetic aperture radars, large-aperture high-gain antennas, large-capacity storage tanks, and solar wings. However, there is currently no detector configuration design that can meet the above-mentioned detection installation requirements. For this reason, it is urgent to carry out the configuration design of the Venus probe related to it to meet the detection requirements. Contents of the invention [0003] The purpose of the present invention is to improve a Venus detector configuration to solve the technical problem in the prior art that the detector configuration cannot meet the needs of Venus detection. [0004] In order to achieve the above object, the object of the present invention is to provide a Venus detect...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G1/10B64G1/44
Inventor 张伟任友良吕凯方宝东王伟
Owner SHANGHAI SATELLITE ENG INST
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