CN114084376A - Kinetic energy penetration type detection device based on star catalogue emission - Google Patents
Kinetic energy penetration type detection device based on star catalogue emission Download PDFInfo
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- CN114084376A CN114084376A CN202111371337.XA CN202111371337A CN114084376A CN 114084376 A CN114084376 A CN 114084376A CN 202111371337 A CN202111371337 A CN 202111371337A CN 114084376 A CN114084376 A CN 114084376A
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- 230000035515 penetration Effects 0.000 title claims abstract description 48
- 238000001514 detection method Methods 0.000 title claims abstract description 36
- 239000007787 solid Substances 0.000 claims abstract description 8
- 238000004891 communication Methods 0.000 claims abstract description 7
- 238000009434 installation Methods 0.000 claims abstract description 7
- 230000007246 mechanism Effects 0.000 claims description 6
- 230000003014 reinforcing effect Effects 0.000 claims description 2
- 238000011065 in-situ storage Methods 0.000 abstract description 4
- 230000005540 biological transmission Effects 0.000 description 5
- 238000000034 method Methods 0.000 description 3
- 230000000149 penetrating effect Effects 0.000 description 3
- 238000012546 transfer Methods 0.000 description 3
- 238000005553 drilling Methods 0.000 description 2
- 230000033001 locomotion Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 241001061260 Emmelichthys struhsakeri Species 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000009189 diving Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000010249 in-situ analysis Methods 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 239000002344 surface layer Substances 0.000 description 1
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/242—Orbits and trajectories
- B64G1/2427—Transfer orbits
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/244—Spacecraft control systems
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/40—Arrangements or adaptations of propulsion systems
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/66—Arrangements or adaptations of apparatus or instruments, not otherwise provided for
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- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Radar, Positioning & Navigation (AREA)
- Automation & Control Theory (AREA)
- Investigation Of Foundation Soil And Reinforcement Of Foundation Soil By Compacting Or Drainage (AREA)
- Measurement Of The Respiration, Hearing Ability, Form, And Blood Characteristics Of Living Organisms (AREA)
Abstract
The invention discloses a kinetic energy penetration type detection device based on star catalogue emission, which comprises an emission shell, a detection device and a control device, wherein an installation cavity is arranged in the emission shell; the penetration body is arranged in the installation cavity and is in data communication connection with the lander; an attitude control device mounted on a side portion of the penetration body; a solids engine mounted at the aft portion of the penetration body; the ejection device is arranged on the launching shell and used for ejecting the penetration body out of the launching shell. Carrying out penetration type in-situ detection or equipment deployment aiming at a high-value detection area by on-orbit data binding; the launching release is carried out by utilizing the ejection mode, and the disturbance to the loading device is adjustable and controllable, so that the scheme has the characteristics of small influence, high flexibility, rapid deployment and the like.
Description
Technical Field
The invention relates to the technical field of in-situ penetration type detection of extraterrestrial celestial bodies, in particular to a kinetic energy penetration type detection device based on star catalogue emission.
Background
At present, extraterrestrial celestial body detection mainly carries out in-situ detection through unmanned landers (including patrols, landers and the like) and carries out in-situ analysis in a manned mode. Because the range of motion of a rover, an astronaut and the like is limited, detection and analysis can be performed only on a small range and a shallow surface layer near a lander.
In order to research the geological parameters of a certain depth range of an extraterrestrial celestial body, rotary drilling tools, astronauts, penetrating diving and other modes are mainly adopted at home and abroad. But mechanical actuation submersion and drilling tool formats require support assistance from landers, patrols, astronauts, and the like. Penetration type submerging detection can realize deep submerging only by improving landing kinetic energy through a free falling body, so certain requirements are provided for the track height, the movement speed, the release posture and the like of a loading device, and the landing precision and the landing area selection are influenced.
Disclosure of Invention
The invention aims to provide a kinetic energy penetration type detection device based on star catalogue emission, so as to solve the technical problem in the background technology.
In order to achieve the purpose, the invention adopts the following technical scheme:
a kinetic energy penetration type detection device based on star catalogue emission comprises:
the launching device comprises a launching shell, a transmission mechanism and a control mechanism, wherein a mounting cavity is arranged in the launching shell;
the penetration body is arranged in the installation cavity and is in data communication connection with the lander;
an attitude control device mounted on a side portion of the penetration body;
a solids engine mounted at the aft portion of the penetration body;
and the ejection device is arranged on the launching shell and is used for ejecting the penetration body out of the launching shell.
In some embodiments, the landing gear further comprises an electrical connector and a connection cable, the electrical connector is arranged on the ejection device, and the penetration body is in data communication with the landing gear through the connection cable and the electrical connector.
In some embodiments, the penetrating body is disposed within the mounting cavity via a coupling mechanism.
In some embodiments, the launch housing is provided with at least one attachment flange, and the launch housing is connected to the landing gear via the attachment flange.
In some embodiments, at least one stiffening ring is provided on the emission housing.
The kinetic energy penetration type detection device based on the star catalogue emission disclosed by the application can bring the following beneficial effects that but not limited to:
the device has no constraint on the orbit parameters of the lander, can perform high-value area analysis by remote measurement after the lander falls on the star catalogue, and reaches a preset detection area by utilizing on-orbit data binding, so that the detection has sufficient remote sensing analysis time, and the remote and deep unmanned detection and deployment can be quickly realized.
Drawings
FIG. 1 is a cross-sectional view of a kinetic energy penetration type detection device based on star catalogue launching according to the present invention;
FIG. 2 is a schematic diagram of a kinetic energy penetration type detection device based on star catalogue emission according to the present invention;
wherein: the method comprises the following steps of 1-launching a shell, 2-penetrating bodies, 3-attitude control devices, 4-solid engines, 5-connecting mechanisms, 6-ejection devices, 7-electric connectors, 8-connecting cables, 9-reinforcing rings, 10-connecting flanges and 11-operating windows.
Detailed Description
In order to make the objects, technical solutions and advantages of the present application more apparent, the present application is described in further detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the present application and are not intended to limit the present application.
On the contrary, this application is intended to cover any alternatives, modifications, equivalents, and alternatives that may be included within the spirit and scope of the application as defined by the appended claims. Furthermore, in the following detailed description of the present application, certain specific details are set forth in order to provide a better understanding of the present application. It will be apparent to one skilled in the art that the present application may be practiced without these specific details.
A kinetic energy penetration type detecting device based on star catalogue emission according to the embodiment of the present application will be described in detail with reference to fig. 1-2. It is to be noted that the following examples are only for explaining the present application and do not constitute a limitation to the present application.
In the embodiment of the application, as shown in fig. 1-2, the invention provides a kinetic energy penetration type detection device based on star catalogue transmission, which comprises a transmission shell 1, a penetration body 2, an attitude control device 3, a solid engine 4, an ejection device 6, an electric connector 7 and a connecting cable 8, wherein the transmission shell is connected with the transmission shell through a cable; an installation cavity is arranged in the transmitting shell 1; the penetration body 2 is arranged in the installation cavity, and the penetration body 2 is in data communication connection with a lander; the attitude control device 3 is arranged on the side part of the penetration body 2; the solid engine 4 is installed at the tail part of the penetration body 2; the ejection device 6 is mounted on the launcher housing 1 for ejecting the penetrating body 2 out of the launcher housing 1.
The launching shell 1, the launching device 6 and the like form a launching device, the penetration body 2, the attitude control device 3, the solid engine 4 and the like form a detector, and the whole body forms a kinetic energy penetration type detection device.
The kinetic energy penetration type detection device is connected with the lander through the connecting flange 10, and mechanical guarantee conditions of uplink launching, track transfer, star surface landing and the like are provided for the detection device. The detector is arranged in the launching device through a connecting mechanism 5, and meets the mechanical conditions during launching and track transfer; the detector is in data communication with the lander through a connecting cable 8 and an electric connector 7, and electrical signal interaction is carried out.
In order to improve the convenience of assembly, the mounting operation of the ejection device 6, the connecting cable 8, the electric connector 7 and the like is performed through the operation window 11; an operating window 11 is mounted on the launcher housing 1 for mounting the ejector 6, the connection cable 8 and the electrical connector 7.
In order to increase the rigidity of the transmitting housing 1, a reinforcing ring 9 is designed on the transmitting housing 1 to improve the modal characteristics of the transmitting housing 1.
The kinetic energy penetration type detection device carries out orbit transfer along with the lander and lands on the surface of the detected extraterrestrial celestial body, calculates and analyzes the position relation between a landing area and an area to be detected by means of a remote sensing analysis result in the process of encircling the extraterrestrial body orbiter or the orbiter and combining the landing position of the lander, and binds related parameters to the detector through a connecting cable 8 and an electric connector 7.
After the data binding is finished, the detector is transmitted out of the transmitting shell 1 through the ejection device 6; according to the bound data, when the detector detects that the height reaches the preset height, ballistic flight is carried out through the attitude control device 3 and the solid engine 4, so that a preset penetration detection area is reached.
By utilizing the kinetic energy of the flight process, the penetration body 2 is penetrated to a certain depth of the extraterrestrial celestial body, and scientific instruments, effective loads and the like arranged in the penetration body 2 carry out related detection analysis and other work on the depth.
The detection position, penetration speed, landing attitude and the like of the detection device do not depend on the track parameters of a loading device (such as a track device, a lander and the like), so that the limitation on the land precision and the landing area is avoided, and penetration type in-situ detection or equipment deployment can be carried out on a high-value detection area through on-track data binding; the launching release is carried out by utilizing the ejection mode, and the disturbance to the loading device is adjustable and controllable, so that the scheme has the characteristics of small influence, high flexibility, rapid deployment and the like.
The above description is only for the purpose of illustrating the preferred embodiments of the present invention and is not to be construed as limiting the invention, and any modifications, equivalents and improvements made within the spirit and principle of the present invention are intended to be included within the scope of the present invention.
Claims (5)
1. A kinetic energy penetration type detection device based on star catalogue emission is characterized by comprising:
the transmitting shell is internally provided with a mounting cavity;
the penetration body is arranged in the installation cavity and is in data communication connection with the lander;
the attitude control device is arranged on the side part of the penetration body;
a solids engine mounted at the aft portion of the penetration body;
the ejection device is arranged on the launching shell and used for ejecting the penetration body out of the launching shell.
2. The kinetic energy penetration detection device based on the star catalogue launching as claimed in claim 1, further comprising an electrical connector and a connecting cable, wherein the electrical connector is arranged on the ejection device, and the penetration body is in data communication with the lander through the connecting cable and the electrical connector.
3. The kinetic energy penetration type detection device based on the star catalogue emission is characterized in that the penetration body is arranged in the installation cavity through a connecting mechanism.
4. The kinetic energy penetration type detection device based on the star catalogue launching as claimed in claim 1, wherein at least one connecting flange is arranged on the launching shell, and the launching shell is connected with the lander through the connecting flange.
5. The kinetic energy penetration type detection device based on the star catalogue emission according to the claim 1, characterized in that at least one reinforcing ring is arranged on the emission shell.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111371337.XA CN114084376B (en) | 2021-11-18 | 2021-11-18 | Kinetic energy penetration type detection device based on star meter emission |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111371337.XA CN114084376B (en) | 2021-11-18 | 2021-11-18 | Kinetic energy penetration type detection device based on star meter emission |
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| CN114084376A true CN114084376A (en) | 2022-02-25 |
| CN114084376B CN114084376B (en) | 2023-12-22 |
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Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2132803C1 (en) * | 1997-12-30 | 1999-07-10 | Галимов Эрик Михайлович | Method of taking soil of planet and device for realization of this method |
| JP2002205698A (en) * | 2001-01-11 | 2002-07-23 | Fuji Heavy Ind Ltd | Astronomical probe |
| CN102879218A (en) * | 2012-09-26 | 2013-01-16 | 浙江大学 | Sampling device of deep-space asteroid sample collection detector |
| CN106428654A (en) * | 2016-11-17 | 2017-02-22 | 上海卫星工程研究所 | Small-sized split type survivable deep space impactor |
| CN108750150A (en) * | 2018-06-19 | 2018-11-06 | 上海卫星工程研究所 | It is a kind of to invade deep small-sized shock penetration device greatly towards super thick ice sheet |
| CN109665117A (en) * | 2019-01-08 | 2019-04-23 | 上海卫星工程研究所 | Percussion separated penetration device |
| CN109677633A (en) * | 2019-01-17 | 2019-04-26 | 上海卫星工程研究所 | A kind of miniature high-speed ram for physical damage objects outside Earth surface texture |
| CN110132634A (en) * | 2019-06-11 | 2019-08-16 | 中国科学院沈阳自动化研究所 | It is a kind of towards celestial body sampling kinetic energy penetration penetrate sampler |
| US10718750B1 (en) * | 2015-01-01 | 2020-07-21 | Reactive Surfaces Ltd., LLP | Life seeking exoplanet penetrator |
| CN111731516A (en) * | 2020-07-31 | 2020-10-02 | 北京控制与电子技术研究所 | Miniaturized survivable intelligent deep space high-speed impactor |
| CN111924134A (en) * | 2020-08-10 | 2020-11-13 | 四川航天系统工程研究所 | Buffering heat insulation structure for penetrating type detection of extraterrestrial celestial body |
-
2021
- 2021-11-18 CN CN202111371337.XA patent/CN114084376B/en active Active
Patent Citations (11)
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| RU2132803C1 (en) * | 1997-12-30 | 1999-07-10 | Галимов Эрик Михайлович | Method of taking soil of planet and device for realization of this method |
| JP2002205698A (en) * | 2001-01-11 | 2002-07-23 | Fuji Heavy Ind Ltd | Astronomical probe |
| CN102879218A (en) * | 2012-09-26 | 2013-01-16 | 浙江大学 | Sampling device of deep-space asteroid sample collection detector |
| US10718750B1 (en) * | 2015-01-01 | 2020-07-21 | Reactive Surfaces Ltd., LLP | Life seeking exoplanet penetrator |
| CN106428654A (en) * | 2016-11-17 | 2017-02-22 | 上海卫星工程研究所 | Small-sized split type survivable deep space impactor |
| CN108750150A (en) * | 2018-06-19 | 2018-11-06 | 上海卫星工程研究所 | It is a kind of to invade deep small-sized shock penetration device greatly towards super thick ice sheet |
| CN109665117A (en) * | 2019-01-08 | 2019-04-23 | 上海卫星工程研究所 | Percussion separated penetration device |
| CN109677633A (en) * | 2019-01-17 | 2019-04-26 | 上海卫星工程研究所 | A kind of miniature high-speed ram for physical damage objects outside Earth surface texture |
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