CN109665117A - Percussion separated penetration device - Google Patents
Percussion separated penetration device Download PDFInfo
- Publication number
- CN109665117A CN109665117A CN201910017426.0A CN201910017426A CN109665117A CN 109665117 A CN109665117 A CN 109665117A CN 201910017426 A CN201910017426 A CN 201910017426A CN 109665117 A CN109665117 A CN 109665117A
- Authority
- CN
- China
- Prior art keywords
- penetration
- instrument section
- stock
- penetration instrument
- percussion
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 230000035515 penetration Effects 0.000 title claims abstract description 171
- 238000009527 percussion Methods 0.000 title claims abstract description 18
- 238000001514 detection method Methods 0.000 claims description 9
- 230000005540 biological transmission Effects 0.000 claims description 7
- 238000005422 blasting Methods 0.000 claims description 7
- 230000004308 accommodation Effects 0.000 claims description 6
- 238000009434 installation Methods 0.000 claims description 3
- 230000037452 priming Effects 0.000 claims description 3
- 238000010586 diagram Methods 0.000 description 9
- 238000001727 in vivo Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- PEDCQBHIVMGVHV-UHFFFAOYSA-N Glycerine Chemical compound OCC(O)CO PEDCQBHIVMGVHV-UHFFFAOYSA-N 0.000 description 1
- 230000001133 acceleration Effects 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 239000012141 concentrate Substances 0.000 description 1
- 238000000354 decomposition reaction Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 230000002452 interceptive effect Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 239000002689 soil Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 239000002344 surface layer Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/10—Artificial satellites; Systems of such satellites; Interplanetary vehicles
- B64G1/105—Space science
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/10—Artificial satellites; Systems of such satellites; Interplanetary vehicles
- B64G1/105—Space science
- B64G1/1064—Space science specifically adapted for interplanetary, solar or interstellar exploration
- B64G1/1071—Planetary landers intended for the exploration of the surface of planets, moons or comets
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- Astronomy & Astrophysics (AREA)
- General Physics & Mathematics (AREA)
- Aviation & Aerospace Engineering (AREA)
- Life Sciences & Earth Sciences (AREA)
- Sustainable Development (AREA)
- Earth Drilling (AREA)
Abstract
The present invention provides a kind of percussion separated penetration devices, including conical shell (1), penetration instrument section fore-stock (2), penetration instrument section apparatus (3), penetration instrument section after-poppet (4), penetration device rear cover (5)；The conical shell (1) is connect with penetration device rear cover (5) by fastener (7), and first receiving space is collectively defined after connection；The penetration instrument section fore-stock (2), penetration instrument section apparatus (3), penetration instrument section after-poppet (4) are located in the first receiving space of conical shell (1) and penetration device rear cover (5) restriction, wherein, the penetration instrument section fore-stock (2) is located at penetration instrument section apparatus (3) front end, and penetration instrument section after-poppet (4) is located at penetration instrument section apparatus (3) rear end；The penetration instrument section apparatus (3) is the device for referring to pierce or penetrate object.The present invention can effectively realize the impact probing to objects outside Earth.
Description
Technical field
The present invention relates to space flight field of detecting, low more particularly to percussion separated penetration device more particularly to a kind of deep space
Fast percussion separated penetration device configuration.
Background technique
The mankind explore diligently to extraterrestrial unknown life and to the future celestial body that can survive, and promote space technology
The means of development and progress, deep space exploration develop to the multimodes combined detections such as circular, landing, celestial body by the initial detection that leaps
The target of detection is also changed to specific substance inside celestial body surface structure to celestial body.
Deep space impact probing is to the efficient means detected inside deep sky object earth's surface.Entered by penetration device
Inside to target celestial body earth's surface after certain depth, the soil regime of target celestial body is detected, signal on penetration device is passed through
The data that detection obtains can be transferred to repeater satellite, finally pass the earth back.But there are the following problems: when penetration device is pushing away
Into under the limited low speed impact of speedup, Penetration Depth shortens, and behind entrance celestial body inside, it will influences the R-T unit of signal
It works normally.
In addition, objects outside Earth stroke speed is in several hundred metre per second (m/s)s, impact acceleration is up to 104G magnitude, to ensure hitting
The process Instrumental of hitting does not destroy, and device also needs have stronger impact resistance.Therefore, device materials need to reasonably be selected
It takes and apparatus structure is rationally designed, realize Penetration Depth demand when guaranteeing to hit while penetration device structural strength, together
When can also realize signal R-T unit normal work.
Summary of the invention
For the defects in the prior art, the object of the present invention is to provide a kind of percussion separated penetration devices.
A kind of percussion separated penetration device provided according to the present invention, including conical shell, penetration instrument section fore-stock, invade
Thorough instrument section apparatus, penetration instrument section after-poppet, penetration device rear cover；The conical shell and penetration device rear cover are connected by fastener
It connects, first receiving space is collectively defined after connection；The penetration instrument section fore-stock, penetration instrument section apparatus, penetration instrument
Section after-poppet is located in the first receiving space that conical shell and penetration device rear cover limit, wherein the penetration instrument Duan Qianzhi
Frame is located at penetration instrument section apparatus front end, and penetration instrument section after-poppet is located at penetration instrument section apparatus rear end；
Wherein, the penetration instrument section apparatus is the device for referring to pierce or penetrate object.
Preferably, the penetration instrument section fore-stock is mainly connected by four 1/4 circular ring parts by double end blasting bolt
It connects to form annulus；
Wherein, the middle part of 1/4 circular ring part is connected with one end of corresponding first support bar；The first support bar
There is angle between extending direction.
Preferably, the penetration instrument section apparatus includes bullet front end, hollow cylinder rear end, bullet front end, open circles
Both cylindricality rear ends collectively define the second accommodation space, are equipped with detection instrument in second accommodation space；
The hollow cylinder rear end is circumferentially with one or more positive stop keys, and wherein positive stop key extending direction is along open circles
The axial direction of cylindricality rear end.
Preferably, the penetration instrument section after-poppet is mainly by the clamping rings group of the one or more second support bars of connection
At；
Wherein, the second support bar and penetration device rear cover are located at the same side of clamping rings.
Preferably, one or more first is provided on 1/4 circular ring part in the penetration instrument section fore-stock to limit
Position slot, penetration instrument section fore-stock are connected by the first limiting slot with the positive stop key of penetration instrument section apparatus.
Preferably, one or more second limiting slots are provided on the clamping rings in the penetration instrument section after-poppet,
Penetration instrument section after-poppet is connected by the second limiting slot with the positive stop key of penetration instrument section apparatus.
Preferably, the conical shell front end is provided with cross channel opening, and penetration instrument section fore-stock passes through the first support
The other end of bar, which is caught in cross channel opening, connects conical shell.
Preferably, the cross channel opening on the conical shell can be recessed inwardly, while be driven by first support bar
Penetration instrument section fore-stock extends out, and the double end blasting bolt of priming penetration instrument section fore-stock junction, which explodes, to be broken, penetration instrument
Muti-piece is resolved into the fracture of device section fore-stock, and penetration instrument section apparatus falls off and separates with conical shell, penetration device rear cover.
Preferably, it is covered after the penetration device and is provided with signal receiving/transmission device, propulsion device, penetration device rear cover passes through second
Support rod is connected with penetration instrument section after-poppet；
The penetration device rear cover is circular slab, and the one or more tanks being uniformly distributed circumferentially are provided on circular slab
Mounting ring, each tank mounting ring one tank of corresponding installation.
Preferably, after the conical shell connects penetration device by the fixed mounting hole that fastener covers after penetration device
Lid.
Compared with prior art, the present invention have it is following the utility model has the advantages that
1, structure of the invention is reasonable, is deep space penetration device suitable for hitting the impact probing task of surface layer under low speed
Structure design provides technological approaches with realization；It is efficiently applied to all kinds of objects outside Earths such as small feature loss, the moon, Mars, Martian satellite
Impact probing.
2, the present invention can be different according to aimed hardness is hit, and dismount different shell mechanisms, realize and rationally change shell
The size shape of structure adapts to different mission requirements.
3, the present invention is by the way that penetration device shell and penetration instrument section separation design, penetration device shelling machine uses cross
Channel opening, internal penetration instrument section fore-stock are made of four parts and are connected with blasting bolt, and utilize support rod and shell ten
Word channel opening is connected, and shell and bracket interfere the penetration of penetration instrument section when avoiding hitting, and penetration instrument voluntarily invades target
In vivo, Penetration Depth demand can be realized under low speed impact.
4, after penetration device of the present invention is hit, signal receiving/transmission device rests on celestial surface with penetration device rear cover, does not influence
The normal work of signal receiving/transmission device.
Detailed description of the invention
Upon reading the detailed description of non-limiting embodiments with reference to the following drawings, other feature of the invention,
Objects and advantages will become more apparent upon:
Fig. 1 is general structure schematic diagram of the invention.
Fig. 2 is general structure schematic diagram of the invention.
Fig. 3 is configuration schematic diagram of the invention.
Fig. 4 is the schematic perspective view of penetration device conical shell of the present invention.
Fig. 5 is the structural schematic diagram of penetration device conical shell of the present invention.
Fig. 6 is the entirety of penetration instrument section fore-stock of the present invention and the structural schematic diagram of building block.
Fig. 7 is the schematic perspective view of penetration instrument section apparatus of the present invention.
Fig. 8 is the structural schematic diagram of penetration instrument section apparatus of the present invention.
Fig. 9 is the structural schematic diagram of penetration instrument section apparatus of the present invention.
Figure 10 is the structural schematic diagram of penetration instrument section after-poppet of the present invention.
Figure 11 is the entirety of penetration device rear cover of the present invention and the structural schematic diagram of building block.
It is shown in figure:
Specific embodiment
The present invention is described in detail combined with specific embodiments below.Following embodiment will be helpful to the technology of this field
Personnel further understand the present invention, but the invention is not limited in any way.It should be pointed out that the ordinary skill of this field
For personnel, without departing from the inventive concept of the premise, several changes and improvements can also be made.These belong to the present invention
Protection scope.
A kind of percussion separated penetration device provided according to the present invention, as shown in Figure 1, including conical shell 1, penetration instrument
Section fore-stock 2, penetration instrument section apparatus 3, penetration instrument section after-poppet 4, penetration device rear cover 5；The conical shell 1 and penetration device
Rear cover 5 is connected by fastener 7, and first receiving space is collectively defined after connection；The penetration instrument section fore-stock 2, penetration
Instrument section apparatus 3, penetration instrument section after-poppet 4 are located in the first receiving space that conical shell 1 and penetration device rear cover 5 limit,
Wherein, the penetration instrument section fore-stock 2 is located at 3 front end of penetration instrument section apparatus, and penetration instrument section after-poppet 4 is located at penetration instrument
3 rear end of device section apparatus；The penetration instrument section apparatus 3 is the device for referring to pierce or penetrate object.
As shown in figure 3, the penetration instrument section fore-stock 2 is mainly exploded by four 1/4 circular ring parts 11 by double end
The connection of bolt 9 forms annulus；Wherein, the middle part of 1/4 circular ring part 11 is connected with one end of first support bar 8；Described first
There is angle between the extending direction of support rod 8；It is arranged on 1/4 circular ring part 11 in the penetration instrument section fore-stock 2
There are one or more first limiting slots 10.Wherein, when double end blasting bolt 9 is hit, can effective explosive decomposition, prevent from interfering
Penetration.
As shown in figure 4, the penetration instrument section apparatus 3 includes bullet front end 12, hollow cylinder rear end 13, the two is common
It defines the second accommodation space, detection instrument is installed in second accommodation space；The hollow cylinder rear end 13 is circumferential
Equipped with one or more positive stop keys 14, wherein axial direction of 14 extending direction of positive stop key along hollow cylinder rear end 13, bullet
Front end 12 is the shape on bullet head.The penetration instrument section apparatus 3, which is mainly responsible for, carries internal detection instrument penetration to target
In vivo；Preferably, 12 diameter of bullet front end is much smaller compared with conical shell 1, and the area that when penetration contacts with earth's surface is small, contact stress
It concentrates, it is easier to bore deep；Hollow cylinder rear end 13 can bear high overload by individual Cushioning Design.
As shown in figure 5, the penetration instrument section after-poppet 4 is mainly by the fixation of the one or more second support bars 16 of connection
Annulus 15 forms；Wherein, the second support bar 16 is located at the same side of clamping rings 15 with penetration device rear cover 5；The penetration
One or more second limiting slots 17 are provided on clamping rings 15 in instrument section after-poppet 4.
Preferably, penetration instrument section fore-stock 2 passes through 14 phase of positive stop key of the first limiting slot 10 and penetration instrument section apparatus 3
Connection；Penetration instrument section after-poppet 4 is connected by the second limiting slot 17 with the positive stop key 14 of penetration instrument section apparatus 3.Penetration
The positive stop key 14 of instrument section apparatus 3 cooperates the first limiting slot 10, penetration instrument section after-poppet 4 on penetration instrument section fore-stock 2
The effect that the second limiting slot 17 on bracket plays circumferential limit and intensity is reinforced.
As shown in Fig. 2, 1 front end of conical shell is provided with cross channel opening 6, penetration instrument section fore-stock 2 passes through the
The other end of one support rod 8, which is caught in cross channel opening 6, is welded to connect conical shell 1；Preferably, conical shell 1 uses big face
Product coniform shell, improves contact area when hitting with objective body earth's surface, limits the whole resistance of intrusion, so that limitation is outer
Shell invades inside objective body, while conical design increases impact stroke and plays certain buffer function, it is made to rest on target
Surface；Preferably, the size of cross channel opening 6 is greater than the outer diameter envelope of internal penetration instrument section apparatus 3, so that ten when being hit
Word channel opening indent reduces and interferes the penetration of penetration instrument section apparatus 3.
As shown in fig. 6, being provided with signal receiving/transmission device 18, propulsion device 21 on the penetration device rear cover 5；The penetration device
Rear cover 5 is circular slab, and the one or more tank mounting rings 19 being uniformly distributed circumferentially, each tank are provided on circular slab
One tank 22 of corresponding installation of mounting ring 19.
Preferably, fixed mounting hole of the conical shell 1 by 12 fixing bolts 7 on penetration device rear cover 5
20 connection penetration device rear covers 5.
When shock, the cross channel opening 6 on the conical shell 1 is recessed inwardly, while being invaded by the drive of first support bar 8
Thorough instrument section fore-stock 2 extends out, and the double end blasting bolt 9 of 2 junction of priming penetration instrument section fore-stock, which explodes, to be broken, penetration instrument
Muti-piece is resolved into the fracture of device section fore-stock 2；Penetration instrument section apparatus 3 falls off and separates with conical shell 1, penetration device rear cover 5, only invades
Thorough instrument section apparatus 3 carries correlation detection instrument penetration with impulse inertia and enters in objective body, penetration difficulty is reduced, outside taper
Shell 1 and the penetration device rear cover 5 for carrying signal receiving/transmission device 18 rest on target surface, and signal receiving/transmission device 18 works normally.
Specific embodiments of the present invention are described above.It is to be appreciated that the invention is not limited to above-mentioned
Particular implementation, those skilled in the art can make a variety of changes or modify within the scope of the claims, this not shadow
Ring substantive content of the invention.In the absence of conflict, the feature in embodiments herein and embodiment can any phase
Mutually combination.
Claims (10)
1. a kind of percussion separated penetration device, which is characterized in that including conical shell (1), penetration instrument section fore-stock (2), invade
Thorough instrument section apparatus (3), penetration instrument section after-poppet (4), penetration device rear cover (5)；The conical shell (1) and penetration device rear cover
(5) it is connected by fastener (7), collectively defines first receiving space after connection；The penetration instrument section fore-stock (2) is invaded
The first appearance that thorough instrument section apparatus (3), penetration instrument section after-poppet (4) are located at conical shell (1) and penetration device rear cover (5) limits
It receives in space, wherein the penetration instrument section fore-stock (2) is located at penetration instrument section apparatus (3) front end, penetration instrument Duan Houzhi
Frame (4) is located at penetration instrument section apparatus (3) rear end；
Wherein, the penetration instrument section apparatus (3) is the device for referring to pierce or penetrate object.
2. percussion separated penetration device according to claim 1, which is characterized in that the penetration instrument section fore-stock (2)
Annulus is mainly formed by double end blasting bolt (9) connection by four 1/4 circular ring parts (11)；
Wherein, the middle part of 1/4 circular ring part (11) is connected with one end of corresponding first support bar (8)；First support
There is angle between the extending direction of bar (8).
3. percussion separated penetration device according to claim 1, which is characterized in that penetration instrument section apparatus (3) packet
Bullet front end (12), hollow cylinder rear end (13) are included, both bullet front end (12), hollow cylinder rear end (13) are common to be limited
Second accommodation space is equipped with detection instrument in second accommodation space；
The hollow cylinder rear end (13) is circumferentially with one or more positive stop keys (14), wherein positive stop key (14) extending direction
Axial direction along hollow cylinder rear end (13).
4. percussion separated penetration device according to claim 1, which is characterized in that the penetration instrument section after-poppet (4)
Mainly it is made of the clamping rings (15) for being connected with one or more second support bars (16)；
Wherein, the second support bar (16) and penetration device rear cover (5) are located at the same side of clamping rings (15).
5. percussion separated penetration device according to claim 2, which is characterized in that the penetration instrument section fore-stock (2)
In 1/4 circular ring part (11) on be provided with one or more first limiting slots (10), penetration instrument section fore-stock (2) passes through
First limiting slot (10) is connected with the positive stop key (14) of penetration instrument section apparatus (3).
6. percussion separated penetration device according to claim 4, which is characterized in that the penetration instrument section after-poppet (4)
In clamping rings (15) on be provided with one or more second limiting slots (17), penetration instrument section after-poppet (4) passes through second
Limiting slot (17) is connected with the positive stop key (14) of penetration instrument section apparatus (3).
7. percussion separated penetration device according to claim 1, which is characterized in that conical shell (1) the front end setting
Have cross channel opening (6), penetration instrument section fore-stock (2) is caught in cross channel opening (6) by the other end of first support bar (8)
Interior connection conical shell (1).
8. percussion separated penetration device according to claim 7, which is characterized in that the cross on the conical shell (1)
Channel opening (6) can be recessed inwardly, while drive penetration instrument section fore-stock (2) to extend out by first support bar (8), and priming is invaded
The double end blasting bolt (9) of thorough instrument section fore-stock (2) junction, which explodes, to be broken, and penetration instrument section fore-stock (2) fracture is decomposed
At muti-piece, penetration instrument section apparatus (3) falls off and separates with conical shell (1), penetration device rear cover (5).
9. percussion separated penetration device according to claim 1, which is characterized in that be arranged on the penetration device rear cover (5)
There are signal receiving/transmission device (18), propulsion device (21)；After penetration device rear cover (5) is by second support bar (16) and penetration instrument section
Bracket (4) is connected；
The penetration device rear cover (5) is circular slab, and the one or more tanks being uniformly distributed circumferentially are provided on circular slab
Mounting ring (19), each tank mounting ring (19) one tank (22) of corresponding installation.
10. percussion separated penetration device according to claim 1, which is characterized in that the conical shell (1) passes through fastening
Fixed mounting hole (20) of the part (7) on penetration device rear cover (5) connects penetration device rear cover (5).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910017426.0A CN109665117B (en) | 2019-01-08 | 2019-01-08 | Impact separation type penetration device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910017426.0A CN109665117B (en) | 2019-01-08 | 2019-01-08 | Impact separation type penetration device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN109665117A true CN109665117A (en) | 2019-04-23 |
| CN109665117B CN109665117B (en) | 2020-07-28 |
Family
ID=66149388
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910017426.0A Active CN109665117B (en) | 2019-01-08 | 2019-01-08 | Impact separation type penetration device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109665117B (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111409872A (en) * | 2020-03-06 | 2020-07-14 | 上海卫星工程研究所 | Integrated separable connecting and mounting bracket suitable for deep space impactor |
| CN111422376A (en) * | 2020-03-06 | 2020-07-17 | 上海卫星工程研究所 | Modular separated survival impactor based on graded protection |
| 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 |
| CN113721303A (en) * | 2021-08-26 | 2021-11-30 | 四川航天系统工程研究所 | Two-stage separation type moon penetrator with buffer device |
| CN114084376A (en) * | 2021-11-18 | 2022-02-25 | 四川航天系统工程研究所 | Kinetic energy penetration type detection device based on star catalogue emission |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5350137A (en) * | 1993-05-19 | 1994-09-27 | General Dynamics Corporation Space Systems Division | Multiple application paraboloid spacecraft structure |
| EP1655223A2 (en) * | 1999-03-22 | 2006-05-10 | McDONNELL DOUGLAS CORPORATION | Satellite dispenser |
| CN105929140A (en) * | 2016-07-11 | 2016-09-07 | 中国科学院沈阳自动化研究所 | High-speed impacting penetrator structure for detecting lunar soil |
| CN106017237A (en) * | 2016-05-30 | 2016-10-12 | 北京理工大学 | Overload measurement protection device resistant to high-speed collisions |
| CN106742078A (en) * | 2016-11-23 | 2017-05-31 | 上海卫星工程研究所 | One kind inflation allosteric type has air celestial body impact probing device from outside deceleration ground |
| CN108820254A (en) * | 2018-06-19 | 2018-11-16 | 上海卫星工程研究所 | A kind of unidirectional resistance to compression can pull shock separated structure |
-
2019
- 2019-01-08 CN CN201910017426.0A patent/CN109665117B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5350137A (en) * | 1993-05-19 | 1994-09-27 | General Dynamics Corporation Space Systems Division | Multiple application paraboloid spacecraft structure |
| EP1655223A2 (en) * | 1999-03-22 | 2006-05-10 | McDONNELL DOUGLAS CORPORATION | Satellite dispenser |
| CN106017237A (en) * | 2016-05-30 | 2016-10-12 | 北京理工大学 | Overload measurement protection device resistant to high-speed collisions |
| CN105929140A (en) * | 2016-07-11 | 2016-09-07 | 中国科学院沈阳自动化研究所 | High-speed impacting penetrator structure for detecting lunar soil |
| CN106742078A (en) * | 2016-11-23 | 2017-05-31 | 上海卫星工程研究所 | One kind inflation allosteric type has air celestial body impact probing device from outside deceleration ground |
| CN108820254A (en) * | 2018-06-19 | 2018-11-16 | 上海卫星工程研究所 | A kind of unidirectional resistance to compression can pull shock separated structure |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111409872A (en) * | 2020-03-06 | 2020-07-14 | 上海卫星工程研究所 | Integrated separable connecting and mounting bracket suitable for deep space impactor |
| CN111422376A (en) * | 2020-03-06 | 2020-07-17 | 上海卫星工程研究所 | Modular separated survival impactor based on graded protection |
| CN111409872B (en) * | 2020-03-06 | 2020-11-24 | 上海卫星工程研究所 | Integrated separable connecting and mounting bracket suitable for deep space 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 |
| CN111924134B (en) * | 2020-08-10 | 2022-03-25 | 四川航天系统工程研究所 | Buffering heat insulation structure for penetrating type detection of extraterrestrial celestial body |
| CN113721303A (en) * | 2021-08-26 | 2021-11-30 | 四川航天系统工程研究所 | Two-stage separation type moon penetrator with buffer device |
| CN113721303B (en) * | 2021-08-26 | 2024-04-12 | 四川航天系统工程研究所 | Two-stage separation moon penetrator with buffer device |
| CN114084376A (en) * | 2021-11-18 | 2022-02-25 | 四川航天系统工程研究所 | Kinetic energy penetration type detection device based on star catalogue emission |
| CN114084376B (en) * | 2021-11-18 | 2023-12-22 | 四川航天系统工程研究所 | Kinetic energy penetration type detection device based on star meter emission |
Also Published As
| Publication number | Publication date |
|---|---|
| CN109665117B (en) | 2020-07-28 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN109665117A (en) | Percussion separated penetration device | |
| CN210037255U (en) | Kinetic energy penetration sampler for planet sampling | |
| US5526752A (en) | Weapon for destruction of deeply buried and hardened targets | |
| US6672218B2 (en) | Self-propelling projectile having a penetrator core | |
| CN110132634B (en) | Kinetic energy penetration sampler for planet sampling | |
| CN106516178A (en) | Series module combining type common impactor configuration | |
| CN108820261A (en) | A kind of separation tripper for slender type ram | |
| Burgay et al. | A Search for Pulsars in Quiescent Soft X-Ray Transients. I. | |
| EP1762815B1 (en) | Munition with seeking fuze | |
| US20150345912A1 (en) | Impulse and Momentum Transfer Devise | |
| Winglee et al. | High velocity penetrators used a potential means for attaining core sample for airless solar system objects | |
| Charters et al. | Penetration dynamics of rods from direct ballistic tests of advanced armor components at 2–3 km/s | |
| US11313652B1 (en) | Underbody kit | |
| CA1277541C (en) | Armour piercing shell | |
| US20020083822A1 (en) | Neutralization chemical injection penetrator | |
| Pilger | China's New YJ-18 Antiship Cruise Missile: Capabilities and Implications for US Forces in the Western Pacific | |
| Galimov | Luna-Glob project in the context of the past and present lunar exploration in Russia | |
| US20030177933A1 (en) | Apparatus and method for penetrating a barrier | |
| Putzar et al. | Screening tests for enhanced shielding against hypervelocity particle impacts for future unmanned spacecraft | |
| CN113375962B (en) | Planet surface remote sampler | |
| HALL | The RemoveDEBRIS space harpoon | |
| TW201734403A (en) | Aerial vehicle with high penetration | |
| EP0807572B1 (en) | Device for destroying drifting mines | |
| Flamini et al. | Rock Elm, USA | |
| CA2807074A1 (en) | Ultimate lifespan multiplier, ultimate telescope disproving big bang theory, and others |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |