CN107150818A - A kind of space junk based on flexible technology and oriented film panel removes towing sail - Google Patents
A kind of space junk based on flexible technology and oriented film panel removes towing sail Download PDFInfo
- Publication number
- CN107150818A CN107150818A CN201710168059.5A CN201710168059A CN107150818A CN 107150818 A CN107150818 A CN 107150818A CN 201710168059 A CN201710168059 A CN 201710168059A CN 107150818 A CN107150818 A CN 107150818A
- Authority
- CN
- China
- Prior art keywords
- towing
- sail
- panel
- oriented film
- space junk
- 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
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G4/00—Tools specially adapted for use in space
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Tents Or Canopies (AREA)
Abstract
A kind of space junk based on flexible technology and oriented film panel of the present invention removes towing sail, belongs to space junk clearance technique field.Towing sail includes scalable beam framework and the towing surface being made up of oriented film plate and towing sail expansion process；Stretching paillon foil panel is folded on a panel；Panel deploys and panel is expanded into final towing face.Towing sail frame structure includes the four airtight extensible canopies of double acting that are symmetrical and having central tube that link together around the corner, and each section of remaining stage extensible canopy is enclosed in central tube；Towing sail surface texture includes nine main panels being made up of highly stretchable stretched film, then the splice panel being made up of identical high scalability stretched film links together；When pulling sail in compact mode, nine main panels are folded on a panel；In intermediate phase, the towing surface of nine main panel expansion to the last.The towing rigging has high packaging efficiency and allows to deploy big towing surface.
Description
Technical field
The present invention relates to the passive chip minimizing technology of towing sail strengthening system, more particularly to it is a kind of based on flexible technology and
The space junk of oriented film panel removes towing sail, belongs to space junk clearance technique field.
Background technology
All spacecrafts for being sent to space all have limited Acceptable life.After their useful life,
Spacecraft and satellite become useless and accumulated in space, produce a large amount of fragments.Unless they are removed or burnt in an atmosphere
Ruin, otherwise spacecraft and satellite are kept on its track, and with the increase of number of tiles, the collision between them can produce more
Fragment.
At present, there is several methods that the spacecraft derailing that can terminate life cycle.The methodical purpose of institute is by near-earth
Point height reduction is sufficiently large so that the point ultimately re-entered to air force.At this point, being applied to spacecraft or satellite
Air force heating and pressure will increase, and spacecraft or satellite will be destroyed in large quantities in an atmosphere.
Nowadays, leading derailing strategy is directed to use with small rocket motor, and electronic tether or air force towing enhancing come
Prevent from entering caused destruction target debris.Small rocket engine can be used at a particular angle and speed pushing away satellite
To the earth, to ensure destruction when reentering.Rocket engine can be used for reduction satellite speed, cause its fall and because
This burns in an atmosphere.Technique make use of the development for the missilery for having reached business level at present.Rocket it is main excellent
Point is to control unloading process by the shooting of accurate angle.However, rocketry is very expensive, weigh very much and technology is multiple
It is miscellaneous：E.g., including make rocket fuel be under pressure before using rocket fuel to be up to 10 years.
Electronic tether is to extend a distance into following conductive strips between derailing spacecraft and the end mass of deployment, this
Segment distance is likely to be several kilometers.Therefore tether technology is related to disposes and pulls the conductor wire from satellite by magnetic field of the earth.
Interaction between tether and magnetic field of the earth produces propulsive force, can be used for raising and reduces satellite altitude track.Generally, it is
The deployment unit of rope system will keep most of dormancy during its main spacecraft being attached movable life-span.When needing derailing,
System will dispose end quality to start derailment course.Electronic tether has potentiality, but in deployment and in the derailment course phase itself
Between need the active control of height.
Pneumatic towing enhancing is related to the increase of air drag.Air drag is pulled with highly reducing, with height
Increase, air is gradually thinning.This solution track strategy is only limitted to LEO.Satellite in this region undergoes fairly limited gas
Dynamic resistance, and because the reduction of satellite velocities caused by air drag is very small.Aerodynamic towing system can be strengthened
Increase air drag so that satellite velocities release the rate reduction of track within the expected time with satellite.
In resistance strengthening system, towing sail is of particular concern.Up to the present, the concept proposed is included by navigating
Its device transports the compact towing sail close to target debris position, and then compact towing sail is attached to target debris, it is last it
Expand to its final surface.The final surface will be responsible for producing resistance removing target debris from its initial position.The towing table
Face is bigger, and device will faster releasing target debris.In view of space limited in spacecraft, towing sail must be with its compressed format
Loading, which has limited the maximum towing surface of towing sail.
It is that the compressed format of device is loaded into spacecraft that the towing sail concept generally proposed, which refers to discharge and extended,.Cause
This, energy is converted to the intermediate phase of its extended mode by towing gear from compaction state, and is favourable.These features are dragged
Higher packaging efficiency will be allowed by draging sail, and this will cause the towing sail on bigger towing surface.
The manufacture of scalable beam and stretching paper tinsel is ripe technology, in many industrial circle applications.Use these skills
The towing sail of art includes the intermediate phase in expansion process, advantageously forms bigger final towing surface.
The content of the invention
Present invention aim to address the expansion process of the towing sail with intermediate phase, it is allowed to higher packaging efficiency and
Bigger towing surface, proposes that a kind of space junk based on flexible technology and oriented film panel removes towing sail.
Towing sail proposed by the present invention includes scalable beam framework and the towing surface being made up of oriented film plate, and drags
Drag the three phases of sail expansion process：First stage, stretching paillon foil panel is folded on a panel；Second stage, panel
Expansion；Phase III, panel is expanded into final towing face.
The purpose of the present invention is achieved through the following technical solutions：
First, the invention discloses the frame structure of towing sail, including four double actings linked together around the corner
Extensible canopy；This four double acting extensible canopies are symmetrical and have central tube, and each section of the extensible canopy in remaining stage is enclosed in central tube
In；Extensible canopy is gas-pressurized that is airtight and being expanded comprising extensible canopy；
Secondly, the invention discloses the towing surface texture for carrying towing sail, it is included by highly stretchable stretched film
Nine main panels being made；This nine main panels are connected to one by the splice panel being made up of identical high scalability stretched film
Rise；When pulling sail in compact mode, nine main panels are folded on a panel；In intermediate phase, nine main panels
Deploy and deploy towing surface to the last；
3rd, the invention discloses attachment means, expanded comprising will capture the net of target chip and be responsible for towing sail
The net of journey；
4th, the invention discloses will pull sail framework, the side that abbreviation framework, towing sail and attachment means link together
Method；There is three types connection：The bolt of the extensible canopy of connection framework, framework-towing surface connection and framework-attachment means connect
Connect；
The course of work that a kind of space junk based on flexible technology and oriented film panel removes towing sail is as follows：
Step 1: towing sail is loaded in spacecraft with its compact mode；In this stage, each section of extensible canopy is enclosed in
Nine main panels in its central tube and towing surface are rolled over for one；
Step 2: when reaching target chip, net is included in the attachment means of transmitting；Once fragment is captured, sail is pulled
It is released and starts expansion；
Step 3: device will be also referred to as expansion pattern from compact mode development to middle or expansion phase, wherein initially folding
Nine main panels on to one will deploy with the extension of extensible canopy；
Step 4: undeployed state, extensible canopy continues to stretch, mainboard expansion, until reaching final surface；
So far, from step one to step 4, a kind of space junk based on flexible technology and oriented film panel is completed
Remove the course of work of towing sail.
Beneficial effect
A kind of space junk based on flexible technology and oriented film panel removes towing sail, and mechanism is manufactured with other spaces
Compare, have the advantages that：
1. towing rigging of the present invention has high packaging efficiency, so as to allow to store several units in spacecraft；
2. towing sail of the present invention is compared with the towing sail without intermediate expansion phase, it is allowed to deploy big towing table
Face；
3. towing sail size of the present invention is easily adapted to the requirement of different derailing tasks:Scalable beam can be by changing
Become series to extend or shorten, and can adapt to stretch the final area of paillon foil panel by changing the original dimension of plate；
It is very light material 4. the towing surface of the present invention is made up of highly stretchable film, the system proposed will
Device than similarity is lighter；
5. because the manufacturing technology of stretching paper tinsel and scalable beam is ripe, this towing rigging of the present invention, which has, is easy to raw
The advantage of production.
Brief description of the drawings
Accompanying drawing represents that mechanism of the present invention manufactures the process of four towing sails；
Accompanying drawing represents that towing sail of the present invention pulls the particular case that surface removes target debris in 50 square meters.For not
Same fragment, can change the size of towing sail with derailing needs needed for adapting to；Fig. 1 is to Fig. 8 outgoing mechanisms and its component parts；
Fig. 9 represents that a kind of space junk based on flexible technology and oriented film panel of the present invention removes the chip of towing sail
Capture, release and expansion process；
Fig. 1 removes the double cropping in towing sail for a kind of space junk based on flexible technology and oriented film panel of the present invention
With the compact mode of extensible canopy；
Fig. 2 removes the double cropping in towing sail for a kind of space junk based on flexible technology and oriented film panel of the present invention
With the contrast between the compact mode and expansion pattern of extensible canopy；
Fig. 3 shows the towing sail framework in compact mode；
Fig. 4 shows the compact comparison between expansion pattern of towing sail framework；
Fig. 5 shows assembled panel sectional before and after towing sail towing panel main panel and towing sail towing panel：
Fig. 6 shows towing surface with the panoramic view of its Three models：
(a) is with folding mode dragging towing surface in Fig. 6；(b) the expansion pattern on surface is pulled for towing sail；(c) it is
Surface is pulled with the towing sail that it deploys pattern；
Fig. 7 is the annexation of towing sail framework-towing sail；Wherein, (a) is towing sail framework-towing sail towing surface
Joint；(b) it is towing sail framework-towing sail attachment means joint；
Fig. 8 shows the towing sail based on flexible technology and oriented film plate, the compact mode removed for space junk；
Fig. 9 shows the capture of fragment and pulls release and the expansion process of sail, is divided into six stages：(a) spacecraft
Complete intersection to manipulate and be aligned with target debris, (b) capture target debris, (c) opens the towing sail container cover, (d) towing
Sail is discharged, and (e) is separated with spacecraft, the towing sail that (f) is removed based on flexible technology and oriented film panel space fragment；
Wherein, the 1- buckets in Fig. 1,2- public affairs piston rods, 3- mother's piston rods；
4- two ends in Fig. 3 have the cylindrical bolt of connecting rod；
(a) in Fig. 5 pulls the expansion pattern of panel main panel for towing sail, wherein：The main towing panels of 5-, (b) towing
Sail；
In Fig. 5：Pull surface splice panel, 7- rectangles towing surface splice panel, 8- angles towing surface composition surface in 6- side
Plate, (c) deploys pattern towing sail towing surface with it；
10 in Fig. 7 be towing sail framework-towing sail towing faced joint；11 be towing sail framework-towing sail connection dress
Put joint；12 in Fig. 8 be attachment means；
In Fig. 9, (a) spacecraft completes rendezvous maneuver and is aligned with target debris, wherein：13- pulls sail container, and 14- is closed
Towing counter door is closed, 15- target debris, (b) captures target debris, wherein：16- captures net, and (c) opens the towing sail container
Lid, wherein：17- opens towing sail container door, and (d) towing sail is discharged, and (e) is separated with spacecraft, and (f) is based on flexible technology and drawing
Stretch the towing sail of film face-plate space junk removing.
Embodiment
Each accompanying drawing will be combined now, be more fully described and removed not based on the disclosed space junk that is used for
The space manufacture mechanism for pulling sail with size manufactures the process of four towing sails.
The towing sail dimension manufactured using mechanism of the present invention can change, i.e., mechanism of the present invention allows manufacture not
With the towing sail of quantity.The positive side (left side) of the X-axis shown in the left and right corresponding diagram mentioned in a particular embodiment and negative
Side (right side).
Embodiment
The present invention is more fully described now with reference to accompanying drawing.Accompanying drawing illustrates towing of the present invention under particular case
Sail, wherein needing 50 square metres of towing surface to remove target debris.
The towing rigging of the oriented film panel removed based on flexible technology and for space junk has three major parts,
Pull sail frame, towing sail face and towing attachment means；And the joint that these parts link together.
Fig. 1 to Fig. 4 shows the different parts and pattern of towing sail framework；
Towing sail framework is made up of four extensible canopies and four cylindrical bolts that extensible canopy links together；Form frame
Four extensible canopies of frame are double acting telescoping cylinders tubulars, in each direction the four-stage of bucket 1 and 30 with 30cm, often
The individual stage is that 10cm length and 1mm are thick.In this manual, term " beam " will be equivalent to " retracting cylinder ".When retracting cylinder contracts in it
During back-shaped formula (Fig. 1), 1/3rd of internal capacity is occupied by the retraction stage of the first bearing of trend, and 1/3rd are prolonged by second
The retraction stage for stretching direction is occupied, and remaining 1/3rd are filled by compressed air.
Two telescoping cylinders carry father's piston rod 2 as most rear class, therefore they are referred to as father's beam, and two other is flexible
The female piston rod 3 of cylinder carrying, therefore they are referred to as female beam；The stage of final stage and remaining 10cm length has identical length.
When retracted, each 50 centimetres of beam length, and when extended, each telescopic cylinder reaches 710cm (Fig. 2).
Fig. 3 shows the towing sail framework in compact model.Two telescoping cylinders on two ends 4 by having connecting rod
Cylindrical bolt link together.This connecting rod is used to towing sail framework being connected to towing sail dragging surface and towing sail connects
Connection device.
Four retracting cylinders are seal members.Each beam includes compressed air, and it is responsible for the extension of telescopic cylinder section.Initially,
In beam retraction pattern, gas occupies 1/3rd of the internal capacity of each telescopic cylinder, and there is provided for prolonging when inflated
Stretch the pressure of cylinder.
Fig. 4 shows the comparison between the contraction of towing sail frame and expansion pattern；
Fig. 5 and Fig. 6 show the different parts and pattern on towing sail surface.The towing surface of sail is pulled by 9 30 centimetres
Towing sail main panel, 40 towing face splice panels and four packing rings for multiplying 30 centimetres are constituted.Pull surface main panel and drag
Surface splice panel is draged all to be made up and link together by adhesive of highly stretchable stretched film.
Fig. 5 (a) shows towing surface main panel with its expansion pattern；Towing surface main panel multiplies 30cm by nine 30cm
Surface 5 constitute, these main panels are united by 40 splice panels, per 20, face.Fig. 5 (b) is shown in it
The towing surface splice panel of the towing sail of expansion pattern.These joint plates are divided into three groups：Square towing surface joint plate 6,
It connects the turning of four towing surface mainboards；Rectangle pulls surface splice panel 7, and it engages two and pulls surface main panel
Both sides；Surface splice panel 8 is pulled with angle, the reinforcer that surface turning is pulled in towing sail is used as.Fig. 5 (c), which is shown, to be in
It deploys the towing sail towing surface of pattern.All towing surface splice panels are attached to towing surface interarea by adhesive
Plate.Four packing rings are combined with four angles on towing sail towing surface.These packing rings are used to connect on the towing surface for pulling sail
It is connected to towing sail framework.
Fig. 6 shows the global view of the Three models on towing surface：Fig. 6 (a) folding modes, the unfolded patterns of Fig. 6 (b)
Deploy pattern with Fig. 6 (c).In its folding mode, nine towing surface main panels are folded on one, and it is flat that this produces 900
Square centimetre of towing surface；In its expansion pattern, main panel expansion, this produces the towing surface of 8.1 square meters；It is unfolded at its
In pattern, towing surface main panel and towing surface splice panel expansion, this produces the surface of 50,41 square meters.Instead of with exhibition
One opened folds towing surface or the contraction towing surface of expansion, based on the flexible technology and stretching removed for space junk
The solution of the towing sail of film face-plate is the combination for the two methods for causing bigger towing sail towing surface.
It is invention dragging based on the flexible technology and oriented film plate removed for space junk to pull sail attachment means 12
Drag the brain of sail.It controls debris catching and towing sail deployment.Two critical piece is four and frame corners is connected into connection
The inertia reel line of device and debris catching net.
Four wires come out from attachment means and are connected to the corner of towing sail frame.Initially, every wire rod is surrounded
Coil winding in inertia reel system, the length for the wire rod that system control discharges at any time.The device bag
Sensor is included, it verifies that the release length of four lines is identical.These lines are responsible for keeping the compact form of sail frame, until target
Fragment is captured.Once expansion process starts, they need to deploy with identical speed so that the extension of cylinder and the stretching, extension of sail
All occur with desired speed.
Pulling sail attachment means includes the net of parcel at an upper portion thereof；Once target debris is had arrived at, towing sail connection dress
Put to project and capture net.
There is two kinds of joint, removed with being used for space junk based on flexible technology and oriented film plate come by Drag
Sail part links together.Fig. 7 show towing sail framework-towing sail towing faced joint (a) and towing sail framework-
Pull sail attachment means joint (b).It is rigid metal member to pull framework-towing sail towing surface engagement, and it will be used to drag
The lower link for the bolt that the beam for draging sail framework is connected to the packing ring for pulling the corner that sail pulls surface is connected.Towing sail framework-drag
It is rigid metal member to drag sail attachment means joint, and it is connected to the beam for pulling sail framework being connected to from towing sail connection dress
The upper connecting rod of the bolt of the end for four one metal wires for putting out, they are connected to them.
The towing rigging that being used for based on flexible technology and oriented film plate, space junk removed have based on drag sail framework and
Pull three kinds of different modes that sail pulls surface modes.The compacted form of the present invention causes the beam for pulling sail framework to retract, and
The towing surface for pulling sail is in its folding mode.The unfolded pattern of the present invention causes the telescopic cylinder for pulling sail framework partly to stretch
Exhibition, and the towing surface of sail is pulled in its unfolded pattern.The expansion pattern of the present invention causes the beam for pulling sail to be extended
And pulling the towing surface of sail has its expansion pattern.Fig. 8 and Fig. 9 (f) are respectively illustrated based on for space junk removal
Flexible technology and oriented film panel towing sail compact model and expansion pattern.
Towing sail based on flexible technology and need to deposit with compressed mode for the oriented film panel that space junk is removed
Storage is in spacecraft.Fig. 9 (a) shows the spacecraft being aligned with target debris, and Fig. 9 (b) shows the capture of target debris.Boat
Towing sail container in its device 13 needs, with the lid with circular cavity 14, once spacecraft is aligned with target debris, to drag
Capture net 16 can be projected by the circular cavity 14 by draging sail attachment means.Fig. 9 (c) shows the opening of towing sail container cover.For
Being used for based on flexible technology and oriented film panel that space junk is removed pulls sail container cover and is also required to opening 17 so that when
The present invention can be released when target debris has been captured.
Fig. 9 (d) shows the release of towing sail, and Fig. 9 (e) shows the separation with spacecraft, and Fig. 9 (f), which is shown, to be based on
The towing sail that the airborne debris of flexible technology and oriented film panel is removed.When the fragment and spacecraft that are connected with towing sail are enough
When remote, towing sail will arrive first at its unfolded pattern, finally reach its expansion pattern.
When the spacecraft for the towboat for being loaded with the removal of the space junk based on flexible technology and oriented film plate has reached that it is opened up
During on-mode, target debris starts derailing.
Described above is presently preferred embodiments of the present invention, and the present invention should not be limited to the embodiment and accompanying drawing institute is public
The content opened.It is every not depart from the lower equivalent or modification completed of spirit disclosed in this invention, both fall within the model that the present invention is protected
Enclose.
Claims (6)
1. a kind of space junk based on flexible technology and oriented film panel removes towing sail, it is characterised in that：Pull sail bag
The towing surface being made containing scalable beam framework and by oriented film plate, and pull the three phases of sail expansion process：First
In the stage, stretching paillon foil panel is folded on a panel；Second stage, panel expansion；Phase III, panel is expanded into finally
Towing face.
2. a kind of space junk based on flexible technology and oriented film panel according to claim 1 removes towing sail,
It is characterized in that：Stretched the invention discloses the frame structure of towing sail, including four double actings linked together around the corner
Contracting beam；This four double acting extensible canopies are symmetrical and have central tube, and each section of the extensible canopy in remaining stage is enclosed in central tube
In；Extensible canopy is gas-pressurized that is airtight and being expanded comprising extensible canopy.
3. a kind of space junk based on flexible technology and oriented film panel according to claim 1 removes towing sail,
It is characterized in that：The invention discloses the towing surface texture for carrying towing sail, it is included by highly stretchable stretched film system
Into nine main panels；This nine main panels are connected to one by the splice panel being made up of identical high scalability stretched film
Rise；When drawing sail in compact mode, nine main panels are folded on a panel；In intermediate phase, nine main panels
Deploy and deploy towing surface to the last.
4. a kind of space junk based on flexible technology and oriented film panel according to claim 1 removes towing sail,
It is characterized in that：The invention discloses attachment means, the net and responsible towing sail process of expansion that will capture target chip are included
Net.
5. a kind of space junk based on flexible technology and oriented film panel according to claim 1 removes towing sail,
It is characterized in that：The invention discloses the method that framework, towing sail and attachment means link together；There is three types company
Connect：The bolt of the extensible canopy of connection framework, framework-towing surface connection and framework-attachment means connection.
6. a kind of space junk based on flexible technology and oriented film panel according to claim 1 removes towing sail,
It is characterized in that：The course of work that a kind of space junk based on flexible technology and oriented film panel removes towing sail is as follows：
Step 1: towing sail is loaded in spacecraft with its compact mode；In this stage, each section of extensible canopy is enclosed in wherein
Nine main panels in heart cylinder and towing surface are rolled over for one；
Step 2: when reaching target chip, net is included in the attachment means of transmitting；Once fragment is captured, towing sail is released
Put and start expansion；
Step 3: device will be from compact mode development to middle or expansion phase, wherein nine masters initially folded on one
Panel will deploy with the extension of extensible canopy；
Step 4: undeployed state, extensible canopy continues to stretch, mainboard expansion, until reaching final surface；
So far, from step one to step 4, complete a kind of space junk based on flexible technology and oriented film panel and remove
Pull the course of work of sail.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710168059.5A CN107150818B (en) | 2017-03-21 | 2017-03-21 | It is a kind of that towing sail is removed based on the space junk of flexible technology and oriented film panel |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710168059.5A CN107150818B (en) | 2017-03-21 | 2017-03-21 | It is a kind of that towing sail is removed based on the space junk of flexible technology and oriented film panel |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107150818A true CN107150818A (en) | 2017-09-12 |
| CN107150818B CN107150818B (en) | 2019-10-18 |
Family
ID=59791774
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710168059.5A Active CN107150818B (en) | 2017-03-21 | 2017-03-21 | It is a kind of that towing sail is removed based on the space junk of flexible technology and oriented film panel |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107150818B (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107719708A (en) * | 2017-09-27 | 2018-02-23 | 西北工业大学深圳研究院 | A kind of capture of space junk and remove device and its method |
| CN109279050A (en) * | 2018-08-29 | 2019-01-29 | 中国空间技术研究院 | A kind of the space-based fragment removing platform and method of the composable reconstruct of modularization solar sail |
| WO2019161298A1 (en) | 2018-02-15 | 2019-08-22 | L'garde, Inc. | Space debris engagement and deorbit system |
| CN110304272A (en) * | 2019-06-25 | 2019-10-08 | 西北工业大学 | Micro-nano satellite tracker and its method for tracing are assembled based on truss |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2092409C1 (en) * | 1993-11-16 | 1997-10-10 | Юрий Владимирович Корягин | Method of cleaning near from space objects and small particles by breaking them and device for realization of this method |
| US20120076629A1 (en) * | 2011-12-06 | 2012-03-29 | Altius Space Machines | Sticky Boom Non-Cooperative Capture Device |
| CN102991731A (en) * | 2012-12-17 | 2013-03-27 | 北京理工大学 | Flying mesh catapulting device for acquiring discarded spacecraft |
| CN106275518A (en) * | 2015-06-01 | 2017-01-04 | 北京空间飞行器总体设计部 | Gas-filled unfolded space junk capturing system and extraterrestrial target catching method |
| CN106335657A (en) * | 2015-07-09 | 2017-01-18 | 北京空间飞行器总体设计部 | Six-traction device space debris net capture system |
-
2017
- 2017-03-21 CN CN201710168059.5A patent/CN107150818B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2092409C1 (en) * | 1993-11-16 | 1997-10-10 | Юрий Владимирович Корягин | Method of cleaning near from space objects and small particles by breaking them and device for realization of this method |
| US20120076629A1 (en) * | 2011-12-06 | 2012-03-29 | Altius Space Machines | Sticky Boom Non-Cooperative Capture Device |
| CN102991731A (en) * | 2012-12-17 | 2013-03-27 | 北京理工大学 | Flying mesh catapulting device for acquiring discarded spacecraft |
| CN106275518A (en) * | 2015-06-01 | 2017-01-04 | 北京空间飞行器总体设计部 | Gas-filled unfolded space junk capturing system and extraterrestrial target catching method |
| CN106335657A (en) * | 2015-07-09 | 2017-01-18 | 北京空间飞行器总体设计部 | Six-traction device space debris net capture system |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107719708A (en) * | 2017-09-27 | 2018-02-23 | 西北工业大学深圳研究院 | A kind of capture of space junk and remove device and its method |
| WO2019161298A1 (en) | 2018-02-15 | 2019-08-22 | L'garde, Inc. | Space debris engagement and deorbit system |
| EP3752423A4 (en) * | 2018-02-15 | 2021-11-17 | L'garde Inc. | Space debris engagement and deorbit system |
| US11713141B2 (en) | 2018-02-15 | 2023-08-01 | L'garde, Inc. | Space debris engagement and deorbit system |
| CN109279050A (en) * | 2018-08-29 | 2019-01-29 | 中国空间技术研究院 | A kind of the space-based fragment removing platform and method of the composable reconstruct of modularization solar sail |
| CN109279050B (en) * | 2018-08-29 | 2020-08-14 | 中国空间技术研究院 | Modular solar sail assembling and reconstructing space-based debris removing platform and method |
| CN110304272A (en) * | 2019-06-25 | 2019-10-08 | 西北工业大学 | Micro-nano satellite tracker and its method for tracing are assembled based on truss |
| CN110304272B (en) * | 2019-06-25 | 2020-09-11 | 西北工业大学 | Micro-nano satellite tracker based on truss assembly and tracking method thereof |
Also Published As
| Publication number | Publication date |
|---|---|
| CN107150818B (en) | 2019-10-18 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN107150818B (en) | It is a kind of that towing sail is removed based on the space junk of flexible technology and oriented film panel | |
| US10458757B1 (en) | Deployable net for an intercepting vehicle | |
| US4214721A (en) | Aircraft collapsible fuel tank | |
| CN105246782B (en) | Emission system and the method for payload module to be assembled to emission system | |
| Howe et al. | MOBITAT2: A mobile habitat based on the trigon construction system | |
| Jenniskens et al. | SHEPHERD: a concept for gentle asteroid retrieval with a gas-filled enclosure | |
| JP2021513933A (en) | Space debris engagement and deorbit system | |
| JPH0624483A (en) | Expanding type container for aircraft transportation and its assembly method | |
| CN106275518A (en) | Gas-filled unfolded space junk capturing system and extraterrestrial target catching method | |
| CN206634203U (en) | A kind of police unmanned plane of investigation type | |
| CN111056051B (en) | Net bag for containing flexible space fly net and folding and containing method of flexible space fly net | |
| CN208021761U (en) | A kind of unmanned plane parachute | |
| CN107726021A (en) | A kind of new unmanned plane filming apparatus of taking photo by plane | |
| CN107264846A (en) | Graphene film parcel space junk cleaning plant and method based on Lorentz force | |
| WO2023071573A1 (en) | Water surface foldable emergency runway | |
| CN110116823B (en) | Recoverable and reusable solid carrier rocket sublevel | |
| CN110481753B (en) | Motorized rapid aerial balloon issuing system | |
| CN106564628A (en) | High-thrust and low-impact flexible air-inflation unfolding separation device and method | |
| CN109229342A (en) | A kind of foldable retractable buffer air bag landing gear and landing concept | |
| EP3770352B1 (en) | A concept of the sdt (self deployable tensegrity) structure for the rapid and precise lifting of helium aerostats, especially into the stratosphere | |
| WO2017215462A1 (en) | Reusable air-launched carrier rocket having no landing leg | |
| CN107226221B (en) | The space of different sizes towing sail for space junk removal manufactures mechanism | |
| CN112693629B (en) | Inflatable blocking line connection capsule shell structure | |
| CN109515752A (en) | A kind of deployable solar array and its compress relieving mechanism | |
| CN206885368U (en) | A kind of unmanned plane camera protection device |
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 |