A Manned Lunar Lander Based on Truss Structure

A truss structure and lander technology, which is applied in the directions of astronautical aircraft, astronautical aircraft landing devices, aircraft, etc., can solve problems such as insufficient carrying capacity, and achieve the effects of avoiding pollution, reducing take-off weight and having a good field of vision.

Active Publication Date: 2022-04-05
BEIJING INST OF SPACECRAFT SYST ENG
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  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] At present, the only lunar lander that has successfully achieved manned missions to the moon at home and abroad is the lunar lander of the "Apollo Project" of the United States, which is launched by the "Saturn V" carrier rocket. Carrying capacity is still nowhere near what the Saturn V was capable of

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  • A Manned Lunar Lander Based on Truss Structure
  • A Manned Lunar Lander Based on Truss Structure
  • A Manned Lunar Lander Based on Truss Structure

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Embodiment Construction

[0037] The present invention will be described in detail below with reference to the accompanying drawings and examples.

[0038] This embodiment provides a manned lunar lander based on a truss structure, which can not only meet the needs of astronauts to land on the moon and leave the moon, but also provide space for the astronauts to live and work; The installation space of box structure, landing buffer mechanism, engine and other load equipment.

[0039] Such as figure 1 and 2 As shown, the manned lunar lander includes: ascent stage 1 and descent stage 2; where, as image 3 As shown, the upgrade 1 includes: a sealed cabin 3, a docking mechanism 4 and an engine bracket 7; as Figure 4 As shown, the descent stage 2 includes: the main truss 10 and the landing engine 13; Figure 5 As shown, the main truss 10 includes: a node ball 15 , a longitudinal rod system 16 , a transverse rod system 17 , a short beam 18 and a carrying docking frame 19 .

[0040]The connection relatio...

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Abstract

The invention discloses a manned lunar surface lander based on a truss structure, which relates to the technical field of spacecraft. The lander can realize test launch and orbit change, which includes: an ascending stage and a descending stage, and the two are connected by a The separation mechanism is connected or separated, and the connection and separation mechanism can realize the connection of the ascending stage and the descending stage in the descending stage and the separation of the ascending stage and the descending stage before ascending; wherein, the descending stage adopts a truss structure, which can support the ascending stage and act as a landing leg , and can be used as an instrument cabin; the upgrade can carry people.

Description

technical field [0001] The invention relates to the technical field of spacecraft, in particular to a manned lunar lander based on a truss structure. Background technique [0002] Manned moon landing is the technological integration and innovative development of the lunar exploration project and manned spaceflight project, and it is also the first step for my country's future manned deep space exploration. The lunar landing and ascending aircraft is the key aircraft for manned lunar exploration. Compared with the unmanned lunar lander, the manned lunar lander needs to meet the life and work needs of the astronauts during the lunar landing and ascent stages, ensure the safety of the astronauts, and install the necessary loads and equipment related to detection. The man-made lunar surface lander is much more difficult than the unmanned lunar exploration project. [0003] At present, the only lunar lander that has successfully realized manned missions to the moon at home and a...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64G1/22B64G1/40B64G1/62B64G1/64
CPCB64G1/22B64G1/40B64G1/402B64G1/62B64G1/646
Inventor 施丽铭柴洪友邓宇华盛聪马凯陈燕成志忠许焕宾赵云鹏
Owner BEIJING INST OF SPACECRAFT SYST ENG
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