Manned space and lunar exploration spacecraft system based on lunar cycle revisiting orbit and exploration method

A technology for aircraft and manned spacecraft, applied in the field of manned spacecraft system design, can solve problems such as high operating cost, complex technology, and lack of implementation, and achieve the effect of strong exploration ability and full mission objectives

A technology for aircraft and manned spacecraft, applied in the field of manned spacecraft system design, can solve problems such as high operating cost, complex technology, and lack of implementation, and achieve the effect of strong exploration ability and full mission objectives

CN102730200AInactive Publication Date: 2012-10-17BEIJING SPACE TECH RES & TEST CENT

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  • Manned space and lunar exploration spacecraft system based on lunar cycle revisiting orbit and exploration method
  • Manned space and lunar exploration spacecraft system based on lunar cycle revisiting orbit and exploration method
  • Manned space and lunar exploration spacecraft system based on lunar cycle revisiting orbit and exploration method

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Embodiment Construction

[0049] The present invention will be described in detail below with reference to the drawings and specific embodiments.

[0050] The invention discloses a manned space and lunar exploration vehicle system based on the lunar cycle revisiting orbit, which can realize manned exploration of the earth-moon space and the moon with the cooperation of an astronaut system, a launch vehicle system and a measurement and control system.

[0051] The manned space and lunar exploration vehicle system consists of four space vehicles: Earth-Moon Space Station (ELS), Lunar Exploration Vehicle (LEM), Manned Spacecraft (CTV), and Cargo Spacecraft (CaTV).

[0052] The following is an example of a relatively complete manned exploration mission to Earth, Moon, space and the Moon:

[0053] (1) The carrier rocket launches the ELS into the Earth-Moon periodic revisit orbit, and becomes a manned Earth-Moon orbit in a large elliptical orbit with a long-term stable operation around the Earth and a half-moon orbit...

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Abstract

The invention discloses a manned space and lunar exploration spacecraft system scheme based on a lunar cycle revisiting orbit and an exploration method. A spacecraft system comprises four spacecrafts which are an earth lunar spaceport (ELS), a lunar exploration module (LEM), a crew transfer vehicle (CTV) and a cargo transfer vehicle (CaTV). With the cooperation of an astronaut system, a carrier rocket system and an exploration and control system, earth lunar space and lunar manned exploration are realized. A relatively entire exploration process of manned space and lunar exploration mission cycle is that the ELS is launched to an earth lunar cycle revisiting orbit by a carrier rocket to become an earth lunar spaceport which surrounds the earth, periodically revisits the moon, and chronically and stably moves on a large oval orbit of which the cycle is half of the lunar orbit cycle; then the lunar exploration module, the crew transfer vehicle and the cargo transfer vehicle are orderly launched to a cycle revisiting orbit by the carrier rocket for rendezvous and docking with the earth lunar spaceport; then the lunar exploration module is separated from the earth lunar spaceport to execute lunar manned field exploration; and finally the lunar exploration module returns to the earth lunar spaceport after finishing the lunar mission, and the crew transfer vehicle is separated from the earth lunar spaceport and then returns to the earth.

Description

Technical field [0001] The invention belongs to the field of manned spacecraft system design, in particular to the field of manned space and lunar exploration, and specifically relates to a manned space and lunar exploration vehicle system and detection method based on the lunar cycle revisiting orbit. Background technique [0002] At present, the international manned space industry is in a new period of development, and the major space powers have aimed at manned moon, asteroid and interplanetary exploration. [0003] Foreign countries have carried out a series of planning and design around the mission goal of manned moon landing, but only the American APOLLO manned moon landing project has been successfully implemented. The detection method of the APOLLO manned lunar landing project is: the flight plan of rendezvous and docking on the lunar orbit is adopted. [0004] (1) The Saturn 5 rocket fired for the first time to send the "Apollo" spacecraft into the orbit of the earth; [000...

Claims

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Application Information

Patent Timeline
17 Oct 2012
Publication
CN102730200A
IPC
B64G1/10
Inventors
杨雷; 闵学龙