Split small manned lunar lander seal

A lander, folio-type technology, applied in the direction of aircraft, aerospace vehicles, aerospace equipment, etc., can solve the problems of increased complexity of the implementation process of the launch vehicle aircraft system specifications and tasks, and achieve the reduction of overall weight and wide observation Field of view, compact structure effect
CN108639382BActive Publication Date: 2020-04-17BEIJING SPACE TECH RES & TEST CENT
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Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
BEIJING SPACE TECH RES & TEST CENT
Publication Date
2020-04-17

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Abstract

The invention relates to a split type small-sized manned lunar surface lander sealed cabin. The split type small-sized manned lunar surface lander sealed cabin comprises a docking mechanism, a passage, a main cabin body and a side scuttle, wherein the docking mechanism, the passage and the main cabin body are connected with each other in sequence; the side scuttle is supported on the main cabin body; the side scuttle comprises a first side scuttle part and a second side scuttle part; the first side scuttle part can be opened in a direction far away from the second side scuttle part; and the second side scuttle part can be opened in a direction far away from the first side scuttle part. According to the split type small-sized manned lunar surface lander sealed cabin, as the side scuttle comprises the first side scuttle part and the second side scuttle part which can oppositely opened, the side scuttle can also be used as a sealed cabin door; and therefore, the floor space of the sealedcabin door in the prior art is saved, the structure of the sealed cabin is made more compact and the light of the sealed cabin is made much lighter.
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Description

technical field

[0001] The invention relates to the technical field of manned space exploration aircraft systems, in particular to a split type small-sized manned lunar lander airtight cabin. Background technique

[0002] Lunar exploration has always been a hot spot in the research and development of space technology around the world. Recently, it has been demonstrated that the number of people and the number of stays in lunar exploration missions have increased in different ways. The overall improvement of mission objectives will make the launch vehicle capability, aircraft system specifications and mission implementation process more complicated. A significant increase. If you consider the mission requirements based on a deep-space orbital space station or a manned moon base, as well as the mission goal of launching multiple repeated moon landings in one launch. With the help of the on-orbit system, the task scale of manned lunar landing and take-off can be flexibly share...

Claims

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