Manned habitation cabin for space exploration

A space detection and space sealing technology, which is applied in the field of manned spaceflight, can solve the problems of difficult transportation of the manned living quarters, and achieve the effect of light weight, reduced weight and small carrying capacity

Active Publication Date: 2018-10-09
BEIJING SPACE TECH RES & TEST CENT
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0003] The purpose of the present invention is to provide a manned habitat for space expl

Method used

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  • Manned habitation cabin for space exploration
  • Manned habitation cabin for space exploration
  • Manned habitation cabin for space exploration

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Embodiment approach

[0031] According to one embodiment of the present invention, the rigid cabin 1 is used to control the operation of the entire manned habitation cabin. In this embodiment, the rigid cabin 1 includes an environmental control system, a thermal control system, a power supply system, and a measurement, control and communication system. The flexible cabin 2 is the living area of ​​the astronauts, including the kitchen and dining room, bedrooms, gymnasium, toilet, etc., and places environmental control and life protection materials. The flexible cabin 2 is relatively large and communicates with the rigid cabin 1 through the hatch. In this embodiment, the rigid cabin 1 is a columnar body, and its opposite ends are provided with docking structures 11 . The docking structure 11 ensures that the manned living cabin of the present invention can be rendezvoused and docked with a manned spaceship, an exploration vehicle, and the like.

[0032] According to an embodiment of the present inve...

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Abstract

The invention relates to a manned habitation cabin for space detection. The manned habitation cabin comprises a rigid cabin (1) and a flexible cabin (2), wherein the rigid cabin (1) is arranged at a central position, and the flexible cabin (2) is arranged surrounding the rigid cabin (1). In the initial state, the flexible cabin (2) is in a retracted state, and in the working state, the flexible cabin (2) is in an unfolded state. By adopting the combined structure of the rigid cabin and the flexible cabin, the advantages of the two structural forms are integrated, and the rigid cabin in the central position is used as a bearing structure and fully satisfies the bearing requirements in the process of carrying launch or orbital maneuvering. The flexible cabin is in a retracted state during the carrying launch or orbital maneuvering process, the occupied space is small, and mass characteristics are relatively definite, so that the flexible cabin in a retracted state is beneficial to the carrying launch or orbital maneuvering process; and the flexible cabin is light in weight, thus the carrying capacity of a carrier is less required, the limitation of the carrying capacity is met, and the carrying cost is further reduced.

Description

technical field [0001] The invention relates to the field of manned spaceflight, in particular to a manned habitation cabin for space exploration. Background technique [0002] With the development of aerospace technology, manned deep space exploration will be further developed and will become a development trend in the future. In the prior art, due to technical limitations such as vehicles, humans can only achieve long-term residence in low-Earth orbit, and the living quarters used for astronauts to reside are small in size and heavy in weight. It is difficult to meet the needs of manned deep space exploration in the future. Therefore, a manned habitat with a larger sealed space is required to ensure that astronauts have a relatively spacious and comfortable living environment during long-term space resident missions. If the existing technology is used to build a larger manned habitat, it will not only be bulky, but also heavy and complex in structure. Not only the existin...

Claims

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Application Information

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IPC IPC(8): B64G1/12B64G1/46
CPCB64G1/12B64G1/46
Inventor 田林张柏楠王平梁鲁彭坤奉振球
Owner BEIJING SPACE TECH RES & TEST CENT
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