A rocket-powered Mars transport aircraft

A technology of transport aircraft and Mars, which is applied in the field of rocket-powered Mars transport aircraft, can solve the problem of low carrying capacity of Mars transport aircraft, and achieve the effects of lowering the center of gravity, efficient completion, and high carrying capacity

Inactive Publication Date: 2018-12-18
NAT UNIV OF DEFENSE TECH
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AI Technical Summary

Problems solved by technology

[0007] The purpose of the present invention is to provide a rocket-powered Mars transporter, which is used to overcome the defects of the low carrying capacity of t...

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  • A rocket-powered Mars transport aircraft
  • A rocket-powered Mars transport aircraft
  • A rocket-powered Mars transport aircraft

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Embodiment Construction

[0030] In order to facilitate the implementation of the present invention, further description will be given below in conjunction with specific examples.

[0031] Such as Figure 1-2 A rocket-powered Mars transporter shown includes a buffer landing system, a power system, a carrying system, a navigation guidance and control system, and an energy system.

[0032] The carrying system includes:

[0033] Truss 1, as the main support frame of the Mars transport aircraft, is in a "cross" layout;

[0034] The top load compartment is arranged on the top of the truss 1 and is not shown in the figure, and is used to carry the Mars rover and infrastructure materials;

[0035] There are multiple bottom load bins 21, which are suspended in a ring form at the bottom of the truss 1, and are used for loading detection equipment and infrastructure equipment.

[0036] By distributing the load, the structure of the Mars transporter is made more compact, and the center of gravity of the Mars t...

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Abstract

The invention provides a rocket-powered Mars transport aircraft, comprising a bearing system,a buffer landing system, a power system, an energy system and a navigation guidance and control system. Thebuffer landing system, the power system, the energy system and the navigation guidance and the control system are arranged on the bearing system. The bearing system comprises a truss, and the power system comprises a main engine arranged on the bottom of the frame. The energy system comprises a high-pressure gas cylinder and a storage tank, wherein the high-pressure gas cylinder is arranged in the middle of the truss, the number of the storage tanks is a plurality of and is arranged at the side of the truss in an annular interval, the high-pressure gas cylinder is communicated with each storage tank through pipelines, and each storage tank is connected with the main engine through pipelines. Adopt modular design, The landing cushion, power system, load bearing system, energy system and navigation guidance and control system are more reasonably installed on the truss, so that the load is more dispersed on the premise of ensuring that the Mars transport aircraft is more compact in structure, and the center of gravity of the Mars transport aircraft is reduced, so that the Mars transport aircraft has higher load bearing capacity. The invention is applied to the field of planetary surface flight.

Description

technical field [0001] The invention relates to a Mars surface vehicle, in particular to a rocket-powered Mars transporter. Background technique [0002] With the development of Mars exploration technology, people's understanding of Mars is gradually deepening. In order to further explore and develop Mars, realizing manned landing on fire has become the next goal of the Mars missions of various countries. Human landing on fire is a key step in the exploration and development of Mars. After landing on fire, there are still many problems to be solved. Including how to efficiently detect unknown areas, how to carry out material delivery and personnel movement, how to ensure personnel safety, etc. The above problems are all related to transportation, so reliable means of transportation is the key to solving the above problems. [0003] At present, there is no professional transportation tool on Mars. The Mars rover that has been put into use is mainly used for exploration. It...

Claims

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Application Information

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IPC IPC(8): B64G1/22B64G1/42B64G1/24
CPCB64G1/22B64G1/24B64G1/42
Inventor 李清廉崔朋林文浩陈兰伟盛立勇肖礼王小波吴继平张家奇
Owner NAT UNIV OF DEFENSE TECH
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