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A manned Mars exploration system and method based on Earth-Mars circular orbit

A technology of circular orbit and detection system, which is applied in the design of spacecraft system and the field of manned spaceflight system, and can solve the problems of poor sustainability and single detection target

Active Publication Date: 2016-08-24
CHINA ACAD OF LAUNCH VEHICLE TECH
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Problems solved by technology

[0011] The technical problem solved by the present invention is: to overcome the shortcomings of the traditional Mars exploration scheme, one mission is similar to the American DRA5.0 mission, one mission alone launches manned aircraft and cargo aircraft, the detection target is single, and the sustainability is poor. The manned Mars exploration system and method of the Mars cyclic orbit can regularly revisit the Earth and Mars through the Earth-Mars cyclic orbit space station

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Embodiment Construction

[0043] The specific implementation manners of the present invention will be further described in detail below in conjunction with the drawings and specific examples.

[0044] At first concept in the present invention is explained as follows:

[0045] Commonly used classifications of orbits for Mars exploration missions can be found in figure 1 .

[0046] The so-called circular orbit is relative to the direct orbit and the parking orbit at both ends. The direct orbit refers to the transfer orbit from the surface of the earth directly to the surface of Mars or the orbit of Mars; the parking orbit at both ends refers to the transfer orbit from the orbit of the earth to the orbit of Mars; An orbit that flies around without stopping. Vehicles operating in cyclic orbits can maintain long-term interplanetary reciprocating flights without the need for orbital maneuvers (or with only minor orbital maneuvers). A circular orbit that does not require the spacecraft itself to maneuver ...

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Abstract

The invention discloses a manned Mars detection system and method based on an earth-Mars circulating orbit. A manned Mars detection aircraft large system comprises an earth-Mars circulating track orbit space station, a manned aircraft, a freight aircraft and other space aircrafts, and realizes manned detection on the Mars and earth-Mars space with the corporation of relevant systems, such as a cosmonaut system, a carrier rocket, a measurement and control system and the like. The system is applied to long-term, persistent and multi-batch manned Mars detection tasks, can realize manned detection tasks on the earth, Mars space and the Mars, and meanwhile provides an ideal research platform for the scientific research on earth and Mars space.

Description

technical field [0001] The invention belongs to the field of spacecraft system design, in particular to the field of manned space and manned Mars exploration in the field of manned spaceflight systems, and specifically relates to a manned Mars detection system and method based on the Earth-Mars cycle orbit, which can be applied to Manned missions to Mars and to the Earth-Mars space. Background technique [0002] The international manned spaceflight industry experienced a low ebb after the "Apollo" exploration mission, until the "Return to the Moon" program of the United States in the new century, which rekindled the dream of manned interstellar exploration by all space powers. [0003] At present, the outer space planets that human science and technology can reach or have the possibility to reach are mainly the moon and Mars. The most in-depth study is the US DRA5.0 (Design Reference Architecture 5.0) manned Mars exploration program. [0004] The basic method of traditiona...

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64G1/10
Inventor 童科伟高朝辉唐庆博吴胜宝申麟彭小波王俊峰时剑波
Owner CHINA ACAD OF LAUNCH VEHICLE TECH
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