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retractable orbital module

A technology of retractable orbit and inner cabin, applied in the direction of artificial satellites, etc., can solve the problems of consuming time, energy and painstaking efforts of scientific and technological personnel, failure to maximize the benefits of launch vehicles, and uneconomical problems

Inactive Publication Date: 2017-11-17
李新亚
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Problems solved by technology

Multiple launches are not economical, and consume a lot of time, energy and effort of a large number of scientific and technical personnel, and the benefits of the launch vehicle have not been maximized

Method used

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Embodiment Construction

[0047] A retractable orbital module is launched into space by a carrier rocket and docked with a known space station, and stays in the air for a long time for astronauts to live or work.

[0048] like Figure 1 to Figure 9 As shown in each figure, the retractable orbital cabin is composed of an inner cabin 1, a middle cabin 2, and an outer cabin 3.

[0049] like figure 1 , figure 2 , image 3 , Figure 4 , Image 6 , Figure 7 , Figure 8 , Figure 9 As shown in each figure, the inner cabin 1 of the retractable orbital cabin is fastened and combined as a whole by the known inner cabin middle section 1a, the known inner cabin front cone section 6, and the known inner cabin docking mechanical device 7, and the axes of these three components coincide; figure 1 , Figure 5 , Image 6 , Figure 8 As shown in each figure, there are n inner cabin bolt holes 1d evenly distributed on the same circumference of the outer circumferential surface of the inner cabin middle secti...

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Abstract

The invention relates to an extension-type orbital module comprising an inner cabin (1), a middle cabin (2) and an outer cabin (3). During the process of lifting off by a carrier rocket, the extension-type orbital module is in a fold-up state and its volume is approximately equal to the volume of the outer cabin (3). After entering the orbit, the extension-type orbital module extends outward, thus the space for astronauts to live or work is significantly enlarged. The use of multiple sealing measures ensures the safety of the astronauts inside the cabins. While constructing a space station of the same scale, launching the extension-type orbital module can reduce the number of launches, save launching costs, and save manpower as well as resources. The astronauts do not have to go out of the cabins while the extension-type orbital module is extending outwards; therefore, the operating procedure is simple, the strength is small, the time is short, no accessories are required to be taken along, and few tools are required to be carried.

Description

technical field [0001] The invention relates to a retractable orbital module, in particular to a retractable orbital module whose effective volume can be increased after it is lifted into the air and docked with a space station. Background technique [0002] At present, the orbital module launched by the carrier rocket and docked with the space station has only one module, and the volume of one module is limited, which cannot accommodate the living and scientific experiments of many astronauts. In order to expand the size of the space station, multiple launches are required. Multiple launches are not economical, and consume a lot of time, energy and effort of a large number of scientific and technical personnel, and the benefits of the launch vehicle have not been maximized. Contents of the invention [0003] The technical problem to be solved by the present invention is to provide a retractable orbital module that can increase the effective volume in space, has simple op...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64G1/12
CPCB64G1/12
Inventor 李新亚
Owner 李新亚
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