CN110963079A - Overhead crane type manned lunar landing aircraft, lunar landing method and application thereof - Google Patents
Overhead crane type manned lunar landing aircraft, lunar landing method and application thereof Download PDFInfo
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Abstract
The invention provides an aerial crane type manned lunar landing aircraft, a lunar landing method and application thereof. The lunar landing airship comprises four parts, namely a lower downgrade part, an upper upgrade part, a brake stage and a landing support mechanism. The manned spacecraft comprises a service cabin and a return cabin. The descending of the lunar rover is powered down by an air crane, after the power is descended to the lunar hovering height, the air crane system is disconnected from other parts of the lunar rover, the lunar rover is placed on the lunar surface through a rope hanging system, then the rope of the air crane system is disconnected from the lunar rover, and the lunar rover flies to the position near the landing point in the horizontal direction to carry out soft landing. Compared with the traditional conventional lunar landing scheme, the lunar landing platform can reduce overload during landing, reduce the structural weight of the lunar landing platform and improve the safety of astronauts during the lunar landing.
Description
Technical Field
The invention discloses a manned lunar landing aircraft, relates to the field of manned spacecrafts, and particularly relates to an aerial crane type manned lunar landing aircraft, a lunar landing method and application thereof.
Background
The manned lunar spacecraft is a manned spacecraft which transports astronauts from the earth to the moon, performs lunar soft landing and then sends the astronauts back to the earth. The manned spacecraft is used for the transportation of astronauts between the earth and the moon, and the flying orbit is earth-moon transfer orbit, circumlunar orbit, moon-earth transfer orbit and returns to the atmosphere. The lunar rover is used for transporting the astronaut from the lunar orbit to the surface of the moon, then taking off from the lunar surface to transport the astronaut back to the lunar orbit and carrying out rendezvous and docking with the manned spacecraft so as to complete the process of transferring the astronaut from the lunar chamber to the manned spacecraft.
Besides carrying astronauts, the lunar airship can carry other loads such as: scientific experimental equipment, manned lunar vehicles, unmanned lunar detectors and the like.
The lunar surface is a vacuum environment without an atmospheric layer, the lunar airship cannot use a parachute to decelerate and land, and the deceleration and the landing need to be carried out through continuous work of a variable thrust rocket engine in the landing process.
At present, only the Apollo lunar airship in the 60-70 th generation of the 20 th century successfully completes manned lunar landing flight tasks. The Apollo airship comprises a service cabin, a command cabin (a returning cabin) and a lunar landing cabin, wherein all cabin sections and astronauts (about 45 tons in total) are launched by a Mars rocket with five numbers at one time and sent into a Earth-moon orbit transfer. The scheme has extremely high requirement on the earth-moon carrying capacity of the rocket due to one-time launching, and has great risk.
The lunar landing bay of the Apollo spacecraft again includes an upper upgrade and a lower downgrade. The descending stage is positioned below the upper stage and used for power descending, and the descending stage is provided with landing legs and used for buffering and supporting during landing. The overload is large when landing, the requirement on the buffering capacity of landing legs is high, the weight of the aircraft is large, the position of a cockpit of an astronaut is high, the astronaut can reach the moon surface only through a ladder, and inconvenience is brought to the astronaut for getting in and out of the cockpit. Meanwhile, the traditional conventional layout can cause the disturbance of lunar dust on the lunar surface during landing, and the influence of lunar dust splashing on the sensor of the upper upgrading and the lower upgrading is difficult to avoid.
Disclosure of Invention
Aiming at the problems, the invention provides an overhead crane type lunar landing mode and a manned lunar landing aircraft based on a lunar orbit rendezvous and docking lunar-rushing flight mode.
The manned lunar spacecraft comprises a manned spacecraft and a lunar spacecraft which adopts an air crane mode to carry out lunar landing, wherein the lunar spacecraft comprises four parts, namely a lower degradation part, an upper upgrading part, a brake stage and a landing support mechanism.
The lunar landing process of the overhead crane type manned lunar landing mode is as follows: (1) the lunar landing airship is launched by the launch vehicle and sent to the earth-moon orbit transfer. (2) The manned spacecraft carrying the astronauts is sent to the earth-moon orbit transfer by the carrier rocket. (3) The lunar landing airship arrives near the moon, is braked and decelerated by the lunar landing airship brake stage into the lunar orbit, and then the brake stage is abandoned. (4) The manned spacecraft then approaches the moon and is braked and slowed down by the service bay engine into the lunar orbit. (5) The manned spacecraft and the lunar spacecraft meet and are in butt joint for the first time on the lunar orbit, and the astronauts enter the ascending lunar chamber of the lunar spacecraft from the returning chamber of the manned spacecraft. (6) The lunar landing airship is separated from the manned airship. And then starting the lunar airship downgrading engine to perform power descent. (7) The lunar terrain is analyzed in the descending process of the lunar airship, and the lunar terrain autonomously searches for a flat area and is dynamically flown to a specific height above a landing point for hovering. (8) The lower degradation of the lunar rover is disconnected from the lunar rover, and the lunar rover is placed on the lunar surface through the rope hanging system. (9) When the four landing legs of the lunar landing chamber are contacted with the lunar surface and loaded, the rope is disconnected with the lunar landing chamber, and then the horizontal direction of downgrading is maneuvered to a position near the landing point and soft landing is carried out. (10) And (4) completing the lunar surface landing process, and taking the astronauts out of the cabin to carry out lunar surface activities. (11) The astronaut returns to the landing bay and the upstroke engine fires, separating from the landing legs and moving away from the moon. (12) The upper upgrade enters the lunar orbit and is jointed with the manned spacecraft, and the astronaut enters a return capsule of the manned spacecraft. (13) After the manned spacecraft is separated from the ascent level, the engine is started to enter the lunar transfer orbit. (14) The manned spacecraft is braked and decelerated, the re-entry capsule is separated from the service capsule, the re-entry capsule enters the earth atmosphere and is recovered, and the manned lunar-landing task is completed.
The manned spacecraft is of a two-stage configuration and comprises a service cabin and a return cabin, wherein the return cabin is approximately a circular truncated cone, the upper part of the return cabin is a channel for a spacecraft to enter and exit the cabin, and an active docking mechanism is installed and used for docking with the lunar landing cabin. The service cabin is cylindrical, and the tail part of the service cabin is provided with an engine.
The lunar airship adopts a three-stage scheme, wherein the first stage is a braking stage and is used for near-moon braking, the second stage is an upper upgrading stage and is used for lunar surface ascending, and the third stage is a descending stage and is used for power descending. The descending stage adopts an air crane mode, the whole body is a cylinder, and 4 engines are arranged on the circumference of the descending stage and used for power descending. The bottom is provided with a winch, and the lunar landing cabin is placed on the lunar surface through a cable. Meanwhile, the lower degrading bottom can be connected with the lunar chamber through explosion bolts. And a plurality of attitude control engines are arranged on the side surface of the lower degradation stage and are used for attitude adjustment during orbit flight and maneuvering flight control during power descent.
The main structure of the ascending sealed cabin is in a horizontal type structure, one end of the ascending sealed cabin is a cabin door for the lunar surface of the astronaut to go out of the cabin, and the other end of the ascending sealed cabin is a passive docking mechanism for docking with the manned spacecraft. One end of the sealed cabin close to the cabin outlet door is an air lock cabin. The upper upgrading bottom is provided with an ascending engine for the lunar surface to take off and enter the circumlunar orbit. The left side and the right side are provided with a posture control engine, a fuel tank and an engine plume protection mechanism. The top is provided with a communication antenna.
The landing buffer structure is used for maintaining the landing stability of the lunar landing cabin, supporting the upgrade on the lunar landing cabin, providing a launching platform for the upgrade to take off from the lunar surface, and has the capability of adjusting the horizontal posture, and the landing legs absorb all or most of energy in the landing buffer process to ensure that the lunar landing cabin is not damaged. The foot pad absorbs partial energy in the process of landing and buffering, and the contact area of the foot pad and the lunar surface is increased.
The brake stage is cylindrical, the tail part is a brake stage main engine, a solar panel is installed on one side of the cylindrical surface to provide power for the lunar airship, and one side of the solar panel faces the sun during space flight, so that a complex unfolding mechanism of the unfoldable solar panel can be avoided.
The invention has the beneficial effects that:
(1) the invention provides an overhead crane type lunar landing mode and manned lunar landing aircraft based on a lunar orbit rendezvous and docking lunar running mode.
(2) In the power descending stage, if the descending is stopped and the lunar climbing is abandoned in case of some emergency, the landing buffer mechanism can be abandoned, the weight is reduced, and the braking engine of the air crane system and the return engine upgraded on the lunar climbing cabin can work simultaneously, so that the lunar climbing cabin can return to the lunar orbit, and the sufficient safety of the lunar climbing cabin is ensured.
(3) The aircraft adopts an air crane mode to place the lunar landing cabin on the lunar surface, so that the overload during landing can be effectively reduced, the comfort of astronauts is improved, and the strength requirement and the structural weight of a landing buffer mechanism are reduced.
(4) The overhead crane type descending level can also carry a camera or other equipment, can also be used for conveying other goods to the lunar surface or hanging and placing lunar surface equipment, and can be reused after fuel is added, so that the cost is reduced.
(5) When the aerial crane type downgrade landing is adopted, the moon dust disturbance on the moon surface can be avoided, and the adverse effect of the splashing of the moon dust on the upgrade and downgrade sensors is reduced.
Drawings
FIG. 1 is a schematic view of a manned spacecraft of an overhead crane-type manned lunar aircraft.
Fig. 2 is a schematic view of a lunar airship of an overhead crane type manned lunar aircraft.
FIG. 3 is a schematic representation of the descent of a lunar spacecraft employing an air crane system.
Fig. 4 is a schematic diagram of upgrading on the lunar landing aircraft.
FIG. 5 is a schematic view of a landing buffer mechanism for a lunar spacecraft.
FIG. 6 is the schematic view of the docking of manned spacecraft and lunar spacecraft on the lunar orbit.
FIG. 7 is a schematic view of the descent of the lunar spacecraft with the lunar chamber positioned to the moon surface by a rope suspension system.
Fig. 8 is a schematic view of an aerial lift truck-type downgrade placing a lunar base bay section or a mobile lunar bay on the moon surface.
In the figure, a manned spacecraft reentry module 1, a manned spacecraft service module 2, a service module main engine 3, a solar panel 4, a posture control engine 5, an active docking mechanism 6, a lunar spacecraft downgrade 7, an ascent stage 8, a landing buffer structure 9, a brake stage 10, a payload 11, a descent stage posture control engine 12, a descent stage main engine 13, a downgrade and ascent stage connecting rod 14, a cable 15, an ascent stage seal module 16, an ascent stage fuel tank 17, a communication antenna 18, an exit hatch door 19, an ascent stage main engine 20, an ascent stage posture control engine 21, an engine plume protection mechanism 22, a handoff docking sensor 23, a passive docking mechanism 24, a hatch door 25, a manual docking cross target 26, landing legs 27, a ladder 28, and landing leg foot pads 29.
Detailed Description
The invention is further described with reference to the following figures and detailed description.
Example 1
The invention provides an aerial crane type manned lunar landing aircraft, which comprises a manned airship and a lunar landing airship, wherein the manned airship and the lunar landing airship are respectively launched and are butted on a circular orbit;
the lunar landing airship is of a three-stage structure, the first stage is a braking stage, is used for near-moon deceleration braking and is positioned at the lowest part of the lunar landing airship; the second level is the upper upgrade, is used for the lunar surface to rise, locate at the middle part of the airship of lunar ascent; the third stage is a descending stage which is used for power descending and is positioned at the uppermost part of the lunar airship; wherein a landing buffer mechanism of the lunar landing cabin is arranged between the upper upgrade and the brake level;
the descending stage adopts an air crane mode, the whole is a cylinder, a plurality of engines are arranged on the circumference of the descending stage and used for power descending, a cable is arranged at the bottom of the descending stage, and the lunar landing cabin is placed on the lunar surface by driving the cable to stretch.
The manned spacecraft comprises a service cabin and a re-entry cabin, wherein an active docking mechanism and rendezvous and docking radar equipment are installed at the top of the re-entry cabin, an engine is installed at the tail of the service cabin, a posture control engine is arranged on the side face of the service cabin, and deployable solar panels are installed on the two sides of the service cabin.
4 or 8 engines are arranged on the circumference of the outer side surface of the lower degradation stage and used for power descending, a winch is arranged at the bottom of the lower degradation stage, and the lunar landing cabin is placed on the lunar surface through 4 cables; the bottom of the lower degradation is connected with the lunar landing cabin through an explosion bolt, and the side surface of the lower degradation is provided with a plurality of attitude control engines for attitude adjustment during orbit flight and maneuvering flight control during power descent.
The ascending stage comprises a sealed cabin which is in a horizontal type structure, one end of the sealed cabin is a cabin door for the lunar surface of the astronaut to go out of the cabin, and the other end of the sealed cabin is a passive docking mechanism for docking with the manned spacecraft;
the device comprises a sealed cabin, a lifting main engine, a posture control engine, a fuel tank and an engine plume protection mechanism, wherein the sealed cabin is provided with an air lock cabin at one end close to an exit cabin door, the lifting main engine is arranged at the bottom of the lifting stage and used for flying off from the lunar surface to enter a lunar orbit, the posture control engine, the fuel tank and the engine plume protection mechanism are arranged on the left side and the right side of the.
The landing buffer mechanism of the lunar landing is internally provided with a plurality of landing legs for maintaining the landing stability of the lunar landing, supporting the upgrade on the lunar landing, providing a launching platform for the upgrade to take off from the lunar surface, and having the capability of adjusting the horizontal posture;
wherein a ladder is arranged on one landing leg close to the cabin door for the astronaut to reach the moon surface, and a radio altitude measuring instrument is arranged at the lower part of the landing buffer mechanism for transmitting the measured altitude data to the downgrade.
Example 2
Based on the lunar landing vehicle, the invention also provides an application of the lunar landing vehicle to downgrade, and the downgrade adopting the air crane system can also be used for moon base construction, transportation of supply equipment to the lunar surface, lunar surface living cabin sections, non-sealed open manned landers and the like. By replenishing the fuel, the downgrade can still be reused after completing a moon landing mission, and is used for hanging transportation of lunar goods and the like.
Example 3
Based on the lunar landing aircraft, the invention also provides an aerial crane type lunar landing method based on intersection and docking of the lunar orbit, and the lunar landing method comprises the following steps:
(1) the lunar landing airship and the manned airship carrying the astronauts are respectively launched by the carrier rocket and sent to the Earth-moon orbit transfer;
(2) the lunar landing airship reaches the vicinity of the moon, the lunar landing airship is braked and decelerated by the brake stage to enter the lunar orbit, and then the brake stage is abandoned;
(3) the manned spacecraft then arrives near the moon, and is braked and decelerated by the engine of the service cabin to enter the lunar orbit;
(4) the manned spacecraft and the lunar spacecraft meet and are in butt joint for the first time on the lunar orbit, and the astronauts enter an ascending lunar chamber of the lunar spacecraft from a returning chamber of the manned spacecraft;
(5) the lunar airship is separated from the manned airship, and then the lunar airship is started to descend the downgrade engine to perform power descent;
(6) the lunar surface terrain is analyzed in the descending process of the lunar airship, a flat area is automatically searched and the lunar airship flies to a specific height above a landing point in a maneuvering mode to hover;
(7) the lower degradation of the lunar rover is disconnected with the lunar rover rigidly, and the lunar rover is placed on the lunar surface through a rope hanging system;
(8) when the four landing legs of the lunar landing chamber are in contact with the lunar surface and are loaded, the rope is disconnected from the lunar landing chamber, and then the landing platform is descended horizontally and maneuverably flies to a position near a landing point and is in soft landing;
(9) and (4) completing the lunar surface landing process, and taking the astronauts out of the cabin to carry out lunar surface activities.
Furthermore, when the lunar landing process is to be terminated in the power descending process, the lunar landing cabin throws off the landing buffer structure, then the upper upgrading engine is started to work simultaneously with the descending engine, and the lunar orbit is returned. After the lower demotion places the lunar landing cabin on the moon surface through the rope hanging system, the horizontal direction of the lower demotion is maneuvered to the position near the landing point and soft landing is carried out, and the camera carried on the lower demotion shoots the lunar surface activities of the astronaut.
The lunar landing method provided by the invention can be applied to other celestial bodies besides the moon.
Example 4
The overhead crane type manned lunar-landing aircraft consists of a manned spacecraft shown in figure 1 and a lunar-landing spacecraft shown in figure 2. Wherein the manned spacecraft is composed of a return capsule 1 and a service capsule 2. An active docking mechanism 6 is installed at the top of the returning capsule 1, deployable solar panels 4 are installed on two sides of the service capsule 2, an attitude control engine 5 is installed on the side face of the service capsule, and a main engine 3 of the service capsule is arranged at the tail of the service capsule.
The lunar airship adopts a three-stage scheme, wherein the first stage is a brake stage 10 for near-moon braking, the second stage is an ascending stage 8 for lunar surface ascending, and the third stage is a descending stage 7 for power descending. The descending stage adopts an air crane mode, the whole body is a cylinder, and 4 engines 13 are arranged on the circumference of the descending stage and used for power descending. The bottom is provided with a winch, and the lunar landing cabin is placed on the lunar surface through four cables 15. And meanwhile, the connecting rod 14 at the bottom of the descending stage is connected with the lunar chamber through an explosive bolt. The lower degrading stage is provided with a plurality of attitude control engines 12 on the side for attitude adjustment during orbit flight and maneuvering flight control during power descent, and the top of the lower degrading stage carries a payload 11.
The upper upgrading sealed cabin 16 has a horizontal structure, one end of the upper upgrading sealed cabin is a cabin door 19 for the lunar surface of the astronaut to go out of the cabin, and the other end of the upper upgrading sealed cabin is a passive docking mechanism 24 for docking with the manned spacecraft. One end of the sealed cabin 16 close to the cabin outlet door is an air lock cabin. The upper upgrade bottom is provided with an upper upgrade engine 20 for the lunar surface to take off and enter the lunar orbit. A plurality of attitude control engines 21, fuel tanks 17, and engine plume prevention mechanisms 22 are mounted on the left and right sides. A communications antenna 18 is mounted on top.
The landing buffer structure is shown in fig. 5, and comprises 4 landing legs 27, which support the landing bay for upgrading, provide a launching platform for the upgrading to take off from the lunar surface, have the capability of adjusting the horizontal attitude, and absorb all or most of energy during the landing buffer process, so as to ensure that the landing bay is not damaged. The foot pad 29 is arranged at the bottom of the landing leg, so that part of energy is absorbed in the landing buffering process, the contact area between the landing leg and the surface of the moon is increased, the pressure on the moon surface during landing is reduced, and the landing leg is prevented from sinking into the moon surface too deeply. The astronaut reaches the moon via a ladder 28.
Example 5
As shown in fig. 8, the landing legs for the landing on moon pool are exchanged for a moonbase bay, a mobile bay or other equipment, which can still be transported from the roundabout to the moon surface using the air crane downgrade.
The foregoing is only a preferred embodiment of the present invention, and it should be noted that modifications can be made by those skilled in the art without departing from the principle of the present invention, and these modifications should also be construed as the protection scope of the present invention.
Claims (10)
1. An aerial crane type manned lunar landing aircraft is characterized in that: the lunar landing aircraft comprises a manned airship and a lunar landing airship which are respectively launched and are butted on the lunar orbit;
the lunar landing airship is of a three-stage structure, the first stage is a braking stage, is used for near-moon deceleration braking and is positioned at the lowest part of the lunar landing airship; the second level is the upper upgrade, is used for the lunar surface to rise, locate at the middle part of the airship of lunar ascent; the third stage is a descending stage which is used for power descending and is positioned at the uppermost part of the lunar airship; wherein a landing buffer mechanism of the lunar landing cabin is arranged between the upper upgrade and the brake level;
the descending stage adopts an air crane mode, the whole is a cylinder, a plurality of engines are arranged on the circumference of the descending stage and used for power descending, a cable is arranged at the bottom of the descending stage, and the lunar landing cabin is placed on the lunar surface by driving the cable to stretch.
2. The aerial lift type manned lunar landing aircraft according to claim 1, wherein: the manned spacecraft comprises a service cabin and a re-entry cabin, wherein an active docking mechanism and rendezvous and docking radar equipment are installed at the top of the re-entry cabin, an engine is installed at the tail of the service cabin, a posture control engine is arranged on the side face of the service cabin, and deployable solar panels are installed on the two sides of the service cabin.
3. The aerial lift type manned lunar landing aircraft according to claim 2, wherein: 4 or 8 engines are arranged on the circumference of the outer side surface of the lower degradation stage and used for power descending, a winch is arranged at the bottom of the lower degradation stage, and the lunar landing cabin is placed on the lunar surface through 4 cables; the bottom of the lower degradation is connected with the lunar landing cabin through an explosion bolt, and the side surface of the lower degradation is provided with a plurality of attitude control engines for attitude adjustment during orbit flight and maneuvering flight control during power descent.
4. The aerial lift type manned lunar landing aircraft according to claim 2, wherein: the ascending stage comprises a sealed cabin which is in a horizontal type structure, one end of the sealed cabin is a cabin door for the lunar surface of the astronaut to go out of the cabin, and the other end of the sealed cabin is a passive docking mechanism for docking with the manned spacecraft;
the device comprises a sealed cabin, a lifting main engine, a posture control engine, a fuel tank and an engine plume protection mechanism, wherein the sealed cabin is provided with an air lock cabin at one end close to an exit cabin door, the lifting main engine is arranged at the bottom of the lifting stage and used for flying off from the lunar surface to enter a lunar orbit, the posture control engine, the fuel tank and the engine plume protection mechanism are arranged on the left side and the right side of the.
5. The aerial lift type manned lunar landing aircraft according to claim 2, wherein: the landing buffer mechanism of the lunar landing is internally provided with a plurality of landing legs for maintaining the landing stability of the lunar landing, supporting the upgrade on the lunar landing, providing a launching platform for the upgrade to take off from the lunar surface, and having the capability of adjusting the horizontal posture;
wherein a ladder is arranged on one landing leg close to the cabin door for the astronaut to reach the moon surface, and a radio altitude measuring instrument is arranged at the lower part of the landing buffer mechanism for transmitting the measured altitude data to the downgrade.
6. The application of descending of the lunar landing vehicle is characterized in that the descending of an air crane system can be used for construction of a lunar base, transportation of supply equipment to the lunar surface, a lunar surface living cabin segment and an unsealed open manned lander;
by replenishing the fuel, the downgrade can still be reused after completing a lunar landing mission for the hanging transportation of lunar cargo.
7. An aerial crane type moon climbing method based on intersection and docking of a circular moon orbit is characterized in that: the lunar landing method comprises the following steps:
(1) the lunar landing airship and the manned airship carrying the astronauts are respectively launched by the carrier rocket and sent to the Earth-moon orbit transfer;
(2) the lunar landing airship reaches the vicinity of the moon, the lunar landing airship is braked and decelerated by the brake stage to enter the lunar orbit, and then the brake stage is abandoned;
(3) the manned spacecraft then arrives near the moon, and is braked and decelerated by the engine of the service cabin to enter the lunar orbit;
(4) the manned spacecraft and the lunar spacecraft meet and are in butt joint for the first time on the lunar orbit, and the astronauts enter an ascending lunar chamber of the lunar spacecraft from a returning chamber of the manned spacecraft;
(5) the lunar airship is separated from the manned airship, and then the lunar airship is started to descend the downgrade engine to perform power descent;
(6) the lunar surface terrain is analyzed in the descending process of the lunar airship, a flat area is automatically searched and the lunar airship flies to a specific height above a landing point in a maneuvering mode to hover;
(7) the lower degradation of the lunar rover is disconnected with the lunar rover rigidly, and the lunar rover is placed on the lunar surface through a rope hanging system;
(8) when the four landing legs of the lunar landing chamber are in contact with the lunar surface and are loaded, the rope is disconnected from the lunar landing chamber, and then the landing platform is descended horizontally and maneuverably flies to a position near a landing point and is in soft landing;
(9) and (4) completing the lunar surface landing process, and taking the astronauts out of the cabin to carry out lunar surface activities.
8. The aerial lift type manned lunar landing method based on lunar orbit intersection docking as claimed in claim 7, wherein: when the lunar landing process is to be terminated in the power descending process, the lunar landing cabin throws off the landing buffer structure, then the upper upgrading engine is started to work simultaneously with the lower upgrading engine, and the upper upgrading engine and the lower upgrading engine return to the lunar orbit.
9. The aerial lift type manned lunar landing method based on lunar orbit intersection docking as claimed in claim 7, wherein: after the lower demotion places the lunar landing cabin on the moon surface through the rope hanging system, the horizontal direction of the lower demotion is maneuvered to the position near the landing point and soft landing is carried out, and the camera carried on the lower demotion shoots the lunar surface activities of the astronaut.
10. Use of the overhead crane-type monthly boarding method according to claim 7, characterized in that: the method can be applied to landing celestial bodies other than the moon.
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| CN201911307501.3A CN110963079A (en) | 2019-12-18 | 2019-12-18 | Overhead crane type manned lunar landing aircraft, lunar landing method and application thereof |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112357118A (en) * | 2020-10-28 | 2021-02-12 | 北京空间飞行器总体设计部 | Manned lunar surface lander based on truss structure |
| CN113104236A (en) * | 2021-02-26 | 2021-07-13 | 北京空间飞行器总体设计部 | Lunar probe suitable for lunar surface automatic sampling return |
| CN113656940A (en) * | 2021-07-08 | 2021-11-16 | 中国人民解放军63919部队 | Manned moon exploration task track design system |
| CN113821867A (en) * | 2021-07-21 | 2021-12-21 | 北京航空航天大学 | Reliability estimation method and estimation system for manned lunar-landing mission spacecraft system |
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2019
- 2019-12-18 CN CN201911307501.3A patent/CN110963079A/en active Pending
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112357118A (en) * | 2020-10-28 | 2021-02-12 | 北京空间飞行器总体设计部 | Manned lunar surface lander based on truss structure |
| CN113104236A (en) * | 2021-02-26 | 2021-07-13 | 北京空间飞行器总体设计部 | Lunar probe suitable for lunar surface automatic sampling return |
| CN113656940A (en) * | 2021-07-08 | 2021-11-16 | 中国人民解放军63919部队 | Manned moon exploration task track design system |
| CN113656940B (en) * | 2021-07-08 | 2022-10-25 | 中国人民解放军63919部队 | Manned moon exploration task track design system |
| CN113821867A (en) * | 2021-07-21 | 2021-12-21 | 北京航空航天大学 | Reliability estimation method and estimation system for manned lunar-landing mission spacecraft system |
| CN113821867B (en) * | 2021-07-21 | 2023-07-14 | 北京航空航天大学 | Reliability estimation method and estimation system for manned lunar-entering task spacecraft system |
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