CN107554824A - A kind of electromagnetic type one-level, booster-missile combination retracting device and method - Google Patents
A kind of electromagnetic type one-level, booster-missile combination retracting device and method Download PDFInfo
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- CN107554824A CN107554824A CN201710845196.8A CN201710845196A CN107554824A CN 107554824 A CN107554824 A CN 107554824A CN 201710845196 A CN201710845196 A CN 201710845196A CN 107554824 A CN107554824 A CN 107554824A
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- 238000011084 recovery Methods 0.000 claims abstract description 112
- 238000005728 strengthening Methods 0.000 claims abstract description 7
- 230000002093 peripheral effect Effects 0.000 claims abstract description 4
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims description 11
- 239000011248 coating agent Substances 0.000 claims description 5
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- 239000007924 injection Substances 0.000 claims description 3
- 239000000203 mixture Substances 0.000 claims description 3
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- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical group [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 1
- 238000002266 amputation Methods 0.000 description 1
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Abstract
The present invention discloses a kind of electromagnetic type one-level, booster-missile combination retracting device, including recovery base center calutron (8) and rocket rocket body (1), it is characterized in that：The recovery base center calutron (8) is fixed on earth's surface, pre-buried concrete strengthening facility is connected below the recovery base center calutron (8), in described recovery base center calutron (8) peripheral circular array, calutron (9) around one group of recovery base is set, pre-buried concrete strengthening facility is connected around the recovery base below calutron (9), calutron (9) is made up of the conductive coil of one group of series connection around the recovery base, calutron (9) is internally provided with calutron inner-core (15) around recovery base around the recovery base.
Description
Technical field
The present invention relates to Aero-Space and rocket launching field, especially a kind of electromagnetic type one-level, booster-missile combination recovery dress
Put and method.
Background technology
As the mankind explore going deep into for space, rocket launching is more and more frequent, and it is a huge work to launch a carrier rocket
Journey, therefore the cost of space launch is high.
In general, the cost of carrier rocket of transmitting includes the following aspects：The development cost of carrier rocket is (single
Valency), the launch cost of carrier rocket, the observing and controlling cost of carrier rocket.The part of composition carrier rocket has very high technology will
Ask, be required for spending substantial amounts of funds in each stage, each stages such as experience beforehand research, production, assembling, tests.Moreover, delivery
The production quantity of rocket can not possibly reach tens thousand of as automobile, and tens pieces up to a hundred pieces of production is quite a lot of, and some is only
Produce several pieces.Can not produce in enormous quantities can undoubtedly increase considerably the cost of single-piece.
The propellant cost, the use cost at launching site and ground that the launch cost of carrier rocket includes consumption are all kinds of attached
Belong to the use cost of facility, also include human cost certainly.Generally, Small Launch Vehicle transmitting once take around 2000~
30000000 dollars；Medium launch vehicle transmitting once takes around 6000~150,000,000 dollars；Large Launch Vehicle is launched once
Take around more than 200,000,000 dollars.
This turns into the important thrust of reusable rocket development.If rocket may be reused, it is possible to drop significantly
The part such as low cost, navigational guidance control, storage tank and the engine of rocket occupies the major part of cost.According to measuring and calculating, if can return
Receive and reuse the first order, fund 80% can be saved；As the second level can also reclaim and reuse, launch cost will in theory
It is down to current 1%.
In the long term, reusable rocket can also make the mankind visit or even migrate turning one's dream into reality for other celestial bodies.
In addition, reusable rocket also has environment protection significance.Environmental Protection in America tissue is issued a research report and claimed before this, rocket
After remains disintegrate completely in ground and water, a large amount of poisonous perchlorate will be remained in soil and current, and this is good for human body
Kang Shifen is unfavorable.
Rocket recovery technology typically has 4 kinds of schemes at present：The first is that parachute vertically declines scheme, and second is power
Counter to push away vertical decline scheme, the third is unpowered gliding flight level landing scheme, and the 4th kind is the horizontal drop of dynamic gliding
Fall scheme.
Following a few point defects be present in existing recovery scheme：First is that controlling is poor, and no hair passes through limited assist device
Ensure direction when rocket falls after rise；Second is that control cost is too high, it is necessary to additional complicated power set, control device, communication
Device；3rd is the posture of rocket rocket body when can not ensure to fall, and easily internal structure is damaged.
The content of the invention
The technical problem to be solved in the present invention is to provide a kind of electromagnetic type one-level, booster-missile combination retracting device, facilitate amputation
Patient's resumes treatment.
The present invention, which adopts the following technical scheme that, realizes goal of the invention：
A kind of electromagnetic type one-level, booster-missile combination retracting device, including recovery base center calutron and rocket rocket body, its
It is characterized in：The recovery base center calutron is fixed on earth's surface, and connection is pre- below the recovery base center calutron
Concrete strengthening facility is buried, electricity around one group of recovery base is set in the recovery base center calutron peripheral circular array
Magnetic device, described reclaim connect pre-buried concrete strengthening facility below calutron around base, electricity around the recovery base
Magnetic device is made up of the conductive coil of one group of series connection, and calutron is internally provided with around recovery base around the recovery base
Calutron inner-core, the recovery base center calutron are made up of the conductive coil of one group of series connection, the recovery base
Ground center calutron is internally provided with recovery base center calutron inner-core, the recovery base center calutron
Top is provided with trampoline, and the trampoline is fixed on ground by one group of trampoline supporting leg of surrounding, and the trampoline surface smear has resistance to
High temperature coating.
As the further restriction of the technical program, umbrella rope one end, the umbrella rope are fixedly connected with the top of the rocket rocket body
The other end is fixedly connected with parachute.
As the further restriction of the technical program, the rocket rocket body outer surface is provided with one group of boosting pedestal, described
One group of air nozzle is provided with boosting pedestal.
As the further restriction of the technical program, rocket body hot-wire coil is provided with the inside of the rocket rocket body outer surface,
The hot-wire coil is made up of the conductive coil largely connected, and the hot-wire coil passes through wire UNICOM battery.
A kind of electromagnetic type one-level, booster-missile combination recovery method, it is characterized in that：
When rocket launching finishes, rocket rocket body is fallen after rise earthward under terrestrial gravitation effect, and major part is excluded by calculating
Interference, rocket rocket body should be fallen after rise to default recovery base or neighbouring position.Connected after rocket rocket body falls certain altitude after rise
Battery, rocket body hot-wire coil are powered, and magnetic field are produced around rocket body hot-wire coil, rocket body hot-wire coil inner facility is converted into
Magnet, at the same reclaim base center calutron, recovery base around calutron be powered, reclaim base around calutron
Inner-core is converted into magnet in the presence of calutron around recovery base, reclaims base center calutron inner-core
Magnet is converted into the presence of base center calutron is reclaimed.By controlling energization direction to ensure rocket rocket body downwards
End and calutron around recovery base center calutron, recovery base are different towards upper end magnetic pole vertically, and there is a natural attraction between the sexes, simultaneously
By controlling the air nozzle on boosting pedestal to be aided in required direction gas injection, it is ensured that rocket rocket body is in disturbing factors such as wind-force
Under the influence of it is in the right direction.
When continuing whereabouts certain altitude, rocket rocket body is nearer apart from ground, opens catapult-launching gear, ejects parachute, umbrella
Rope, change recovery base center calutron energization direction, in parachute, umbrella rope and the effect for reclaiming base center calutron
Lower rocket rocket body falling speed reduces, and is made a circle in terrestrial gravitation and week around recovery base rocket arrow in the presence of calutron
Body falling direction is correct.
When continuing whereabouts certain altitude, rocket rocket body changes recovery base center calutron, recovery base close to trampoline
Surrounding calutron energization direction, making rocket rocket body and recovery base center calutron, there is a natural attraction between the sexes, utilizes terrestrial gravitation, fire
The gravitation of arrow rocket body self inertia and rocket rocket body and recovery base center calutron ensures that rocket rocket body falling direction is correct,
Make rocket rocket body and recovery base around calutron identical charges repel each other, using rocket rocket body and reclaim base around calutron it is same
Property is repelled each other and rocket rocket body speed is declined rapidly.
When continuing whereabouts certain altitude, rocket rocket body into contact with trampoline, changes recovery base center calutron, returned
Calutron energization direction around base is received, making rocket rocket body and recovery base center calutron, identical charges repel each other, makes rocket arrow
Identical charges repel each other for calutron around body and recovery base, and when distance is closeer closer to magnetic induction line between the two, resistance is bigger, when
Trampoline can also bring larger resistance to rocket rocket body after rocket rocket body contact trampoline, when rocket rocket body speed reduces to 0 metre per second (m/s), stop
Non-return is received calutron around base and is powered, and changes recovery base center calutron energization direction, rests on rocket rocket body
On trampoline, now between trampoline elastic force, rocket rocket body self gravitation and rocket rocket body and recovery base center calutron
Gravitation keeps balance, rocket rocket body remains stationary on trampoline.
Recovery is completed.
Compared with prior art, the advantages and positive effects of the present invention are：
1) accuracy in direction when ensure that whereabouts by the Magnetic Control of calutron multiple directions.
2) cost is relatively low, it is only necessary to adds coil and communication control unit in rocket body, does not interfere with rocket rocket body structure, no
Weight can be increased.
3) direction of magnetic force, magnetic pole is ensure that by the direction of coil, it is ensured that rocket body is fallen with vertical posture, is prevented
Occur tilting, damage.
Brief description of the drawings
Fig. 1 is rocket rocket body structure principle schematic；
Fig. 2 is recovery base calutron distribution schematic diagram；
Fig. 3 is exclusion principle schematic diagram when rocket body falls；
Fig. 4 is attraction principle schematic diagram when rocket body falls；
Fig. 5 is apparatus structure schematic diagram when rocket body falls；
Fig. 6 is rocket body whereabouts near-earth energization Impact direction schematic diagram；
Energization Impact direction schematic diagram when Fig. 7 is rocket body whereabouts contact trampoline；
Fig. 8 is energization Impact direction schematic diagram when rocket body falling speed is zero.
In figure：1st, rocket rocket body, 2, rocket body hot-wire coil, 3, boosting pedestal, 4, air nozzle, 5, parachute, 6, umbrella rope, 7,
Battery, 8, recovery base center calutron, 9, calutron around recovery base, 10, trampoline, 11, trampoline supporting leg, 12,
High-temperaure coating, 13, rocket body hot-wire coil inner facility, 14, recovery base center calutron inner-core, 15, recovery base
Calutron inner-core around ground.
Embodiment
Below in conjunction with the accompanying drawings, the specific embodiment of the present invention is described in detail, it is to be understood that of the invention
Protection domain do not limited by embodiment.
As Figure 1-Figure 8, the present invention includes recovery base center calutron 8 and rocket rocket body 1, it is characterized in that：Institute
State recovery base center calutron 8 and be fixed on earth's surface, the lower section of recovery base center calutron 8 connects pre-buried concrete
Facility is reinforced, calutron around one group of recovery base is set in the recovery base center calutron 8 peripheral circular array
9, described reclaim connects pre-buried concrete strengthening facility below calutron 9 around base, electromagnetic installing around the recovery base
Put 9 to be made up of the conductive coil of one group of series connection, calutron 9 is internally provided with electricity around recovery base around the recovery base
Magnetic device inner-core 15, strengthens magnetic force during energization, the recovery base center calutron 8 by one group of series connection conductive coil
Composition, the recovery base center calutron 8 is internally provided with recovery base center calutron inner-core 14, during energization
Strengthen magnetic force, the top of recovery base center calutron 8 is provided with trampoline 10, one group of bullet that the trampoline 10 passes through surrounding
Net supporting leg 11 is fixed on ground, and the surface smear of trampoline 10 has a high-temperaure coating 12, and the high-temperaure coating 12 is preventing
Rocket rocket body 1 falls at a high speed produces a large amount of focuses combustions trampoline 10 with air friction.
The top of rocket rocket body 1 is fixedly connected with the one end of umbrella rope 6, and the other end of umbrella rope 6 is fixedly connected with parachute 5, not
The parachute 5, umbrella rope 6 are collected in inside the rocket rocket body 1 during use, and the parachute 5, the lower section of umbrella rope 6 set ejection
Device, the ejectable of rocket rocket body 1 is opened during use and goes out the parachute 5, umbrella rope 6.
The outer surface of rocket rocket body 1 is provided with one group of boosting pedestal 3, and one group of jet is provided with the boosting pedestal 3
Mouth 4, the air nozzle 4 can be rotated in the case where motor or other devices drive, and the rocket rocket body 1 is sprayed by the air nozzle 4
The thrust that body of emanating is brought realizes the regulation of position.
It is provided with rocket body hot-wire coil 2 on the inside of the outer surface of rocket rocket body 1, the hot-wire coil 2 is by largely connecting
Conductive coil forms, and the hot-wire coil 2 is by wire UNICOM battery 7, the rocket body inside the rocket rocket body 1 when energized
Hot-wire coil inner facility 13 can serve as iron core enhancing magnetic force.
The present invention workflow be：When rocket launching finishes, rocket rocket body 1 is fallen after rise to ground under terrestrial gravitation effect
Face, most of interference is excluded by calculating, rocket rocket body 1 should be fallen after rise to default recovery base or neighbouring position.Work as rocket
Rocket body 1 connects battery 7 after falling certain altitude after rise, and rocket body hot-wire coil 2 is powered, and magnetic field is produced around rocket body hot-wire coil 2,
Rocket body hot-wire coil inner facility 13 is converted into magnet；Base center calutron 8 is reclaimed simultaneously, reclaims electromagnetic installing around base
Put 9 to be powered, reclaim calutron inner-core 15 around base and be converted into the presence of calutron 9 around recovery base
Magnet, recovery base center calutron inner-core 14 are converted into magnet in the presence of base center calutron 8 is reclaimed.
By control energization direction ensure rocket rocket body 1 hold and reclaim downwards base center calutron 8, recovery base around electricity
Magnetic device 9 is different towards upper end magnetic pole vertically, and there is a natural attraction between the sexes, while by controlling the air nozzle 4 on boosting pedestal 3 to required direction
Gas injection aids in, it is ensured that rocket rocket body 1 is in the right direction under the influence of the disturbing factors such as wind-force.
When continuing whereabouts certain altitude, rocket rocket body 1 is nearer apart from ground, open catapult-launching gear, eject parachute 5,
Umbrella rope 6, change recovery base center calutron 8 energization direction, in parachute 5, umbrella rope 6 and recovery base center calutron
The falling speed of rocket rocket body 1 reduces in the presence of 8, is made a circle in terrestrial gravitation and week and reclaims the work of calutron 9 around base
It is correct with the lower falling direction of rocket rocket body 1.As shown in Figure 3.
When continuing whereabouts certain altitude, rocket rocket body 1 is close to trampoline 10, as shown in fig. 6, changing recovery base center electromagnetism
The energization direction of calutron 9 around device 8, recovery base, makes rocket rocket body 1 and recovery 8 different in nature phase of base center calutron
Inhale, as shown in figure 8, utilizing terrestrial gravitation, the self inertia of rocket rocket body 1 and rocket rocket body 1 and recovery base center calutron 8
Gravitation ensure that rocket 1 falling direction of rocket body is correct, make around rocket rocket body 1 and recovery base that identical charges repel each other for calutron 9, it is sharp
With calutron 9 around rocket rocket body 1 and recovery base, identical charges repel each other the speed of rocket rocket body 1 is declined rapidly.As shown in Figure 5.
When continuing whereabouts certain altitude, rocket rocket body 1 into contact with trampoline 10, changes recovery base center calutron
8th, the energization direction of calutron 9 around base is reclaimed, making rocket rocket body 1 and recovery base center calutron 8, identical charges repel each other, makes
Identical charges repel each other for calutron 9 around rocket rocket body 1 and recovery base, as shown in Figure 7.When distance is closer to magnetic strength between the two
Line is closeer, and resistance is bigger, and trampoline 10 also can bring larger resistance to rocket rocket body 1 after rocket rocket body 1 contacts trampoline 10.Work as fire
The speed of arrow rocket body 1 reduces to 0 metre per second (m/s), stops calutron 9 around recovery base and is powered, changes recovery base center calutron
8 energization directions, as shown in figure 8, making rocket rocket body 1 rest on trampoline 10, now the elastic force of trampoline 10, rocket rocket body 1 itself are heavy
Gravitation between power and rocket rocket body 1 and recovery base center calutron 8 keeps balance, and rocket rocket body 1 is on trampoline 10
Remains stationary.
The positional information of rocket coordinates satellite fix, radar fix and sensor positioning etc. to calculate by central processing system
It is determined that this is prior art, here is omitted；The commutation of calutron circuit in central processing system control circuit by opening
The Push And Release of pass realizes, this is that here is omitted for the technological means commonly used of those skilled in the art.
Recovery is completed.
Disclosed above is only the specific embodiment of the present invention, and still, the present invention is not limited to this, any ability
What the technical staff in domain can think change should all fall into protection scope of the present invention.
Claims (5)
1. a kind of electromagnetic type one-level, booster-missile combination retracting device, including recovery base center calutron (8) and rocket rocket body
(1), it is characterized in that：The recovery base center calutron (8) is fixed on earth's surface, the recovery base center calutron
(8) lower section connects pre-buried concrete strengthening facility, and one is set in described recovery base center calutron (8) peripheral circular array
Group reclaims calutron (9) around base, and connection pre-buried concrete strengthening in calutron (9) lower section is set around the recovery base
Apply, calutron (9) is made up of the conductive coil of one group of series connection around the recovery base, electromagnetic installing around the recovery base
Put (9) be internally provided with recovery base around calutron inner-core (15), it is described recovery base center calutron (8) by
The conductive coil composition of one group of series connection, the recovery base center calutron (8) are internally provided with recovery base center electromagnetism
Device inner-core (14), recovery base center calutron (8) top are provided with trampoline (10), and the trampoline (10) is logical
One group of trampoline supporting leg (11) for crossing surrounding is fixed on ground, and trampoline (10) surface smear has high-temperaure coating (12).
2. electromagnetic type one-level according to claim 1, booster-missile combination retracting device, it is characterized in that：The rocket rocket body (1)
Top is fixedly connected with umbrella rope (6) one end, and umbrella rope (6) other end is fixedly connected with parachute (5).
3. electromagnetic type one-level according to claim 1 or 2, booster-missile combination retracting device, it is characterized in that：The rocket rocket body
(1) outer surface is provided with one group of boosting pedestal (3), and one group of air nozzle (4) is provided with the boosting pedestal (3).
4. electromagnetic type one-level according to claim 3, booster-missile combination retracting device, it is characterized in that：The rocket rocket body (1)
Rocket body hot-wire coil (2) is provided with the inside of outer surface, the hot-wire coil (2) is made up of the conductive coil largely connected, described
Hot-wire coil (2) passes through wire UNICOM battery (7).
5. electromagnetic type one-level according to claim 4, booster-missile combination recovery method, it is characterized in that：
When rocket launching finishes, rocket rocket body (1) is fallen after rise earthward under terrestrial gravitation effect, and most of do is excluded by calculating
Disturb, rocket rocket body (1) should be fallen after rise to default recovery base or neighbouring position.After rocket rocket body (1) falls certain altitude after rise
Battery (7) is connected, rocket body hot-wire coil (2) is powered, and magnetic field, rocket body hot-wire coil are produced around rocket body hot-wire coil (2)
Inner facility (13) is converted into magnet, at the same reclaim base center calutron (8), calutron (9) is equal around recovery base
It is powered, reclaims calutron inner-core (15) around base and be converted into the presence of calutron (9) around recovery base
Magnet, recovery base center calutron inner-core (14) are converted into the presence of recovery base center calutron (8)
Magnet.By controlling energization direction to ensure that rocket rocket body (1) is held and recovery base center calutron (8), recovery downwards
Calutron (9) is different towards upper end magnetic pole vertically around base, and there is a natural attraction between the sexes, while by controlling the spray on boosting pedestal (3)
Valve (4) aids in required direction gas injection, it is ensured that rocket rocket body (1) is in the right direction under the influence of the disturbing factors such as wind-force.
When continuing whereabouts certain altitude, rocket rocket body (1) is nearer apart from ground, open catapult-launching gear, eject parachute (5),
Umbrella rope (6), change recovery base center calutron (8) energization direction, in parachute (5), umbrella rope (6) and recovery base center
Rocket rocket body (1) falling speed reduces in the presence of calutron (8), is made a circle in terrestrial gravitation and week and reclaims electricity around base
Rocket rocket body (1) falling direction is correct in the presence of magnetic device (9).
When continuing whereabouts certain altitude, rocket rocket body (1) changes recovery base center calutron (9), returned close to trampoline (10)
Calutron (9) energization direction around base is received, making rocket rocket body (1) and recovery base center calutron (8), there is a natural attraction between the sexes,
Utilize terrestrial gravitation, rocket rocket body (1) self inertia and rocket rocket body (1) and the gravitation of recovery base center calutron (8)
Ensure that rocket rocket body (1) falling direction is correct, make around rocket rocket body (1) and recovery base that identical charges repel each other for calutron (9), it is sharp
With calutron (9) around rocket rocket body (1) and recovery base, identical charges repel each other rocket rocket body (1) speed is declined rapidly.
When continuing whereabouts certain altitude, rocket rocket body (1) into contact with trampoline (10), changes recovery base center calutron
(8) calutron (9) energization direction around base, is reclaimed, makes rocket rocket body (1) and recovery base center calutron (8) same
Property repel each other, make around rocket rocket body (1) and recovery base that identical charges repel each other for calutron (9), when distance is closer between the two
Magnetic induction line is closeer, and resistance is bigger, and trampoline (10) can also be brought to rocket rocket body (1) after rocket rocket body (1) contacts trampoline (10)
Larger resistance, when rocket rocket body (1) speed reduces to 0 metre per second (m/s), calutron (9) is powered around stopping recovery base, changes back
Receive base center calutron (8) energization direction, rocket rocket body (1) is rested on trampoline (10), now trampoline (10) elastic force,
Gravitation between rocket rocket body (1) self gravitation and rocket rocket body (1) and recovery base center calutron (8) keeps flat
Weighing apparatus, rocket rocket body (1) remains stationary on trampoline (10).
Recovery is completed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710845196.8A CN107554824A (en) | 2017-09-19 | 2017-09-19 | A kind of electromagnetic type one-level, booster-missile combination retracting device and method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710845196.8A CN107554824A (en) | 2017-09-19 | 2017-09-19 | A kind of electromagnetic type one-level, booster-missile combination retracting device and method |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107554824A true CN107554824A (en) | 2018-01-09 |
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ID=60981293
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710845196.8A Pending CN107554824A (en) | 2017-09-19 | 2017-09-19 | A kind of electromagnetic type one-level, booster-missile combination retracting device and method |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108592711A (en) * | 2018-04-10 | 2018-09-28 | 合肥凯石投资咨询有限公司 | The recyclable reuse composite structure in carrier rocket end |
| CN109436384A (en) * | 2018-12-04 | 2019-03-08 | 燕山大学 | Manipulator for rocket recycling |
| CN110171582A (en) * | 2019-06-03 | 2019-08-27 | 哈尔滨工业大学 | Spacecraft Recovery electromagnetic damping device |
| CN110185732A (en) * | 2019-06-03 | 2019-08-30 | 哈尔滨工业大学 | Spacecraft Recovery linear electromagnetic damping unit |
| CN110282160A (en) * | 2019-06-28 | 2019-09-27 | 中国科学院电工研究所 | Tubaeform electromagnetic type rocket landing recyclable device |
-
2017
- 2017-09-19 CN CN201710845196.8A patent/CN107554824A/en active Pending
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108592711A (en) * | 2018-04-10 | 2018-09-28 | 合肥凯石投资咨询有限公司 | The recyclable reuse composite structure in carrier rocket end |
| CN109436384A (en) * | 2018-12-04 | 2019-03-08 | 燕山大学 | Manipulator for rocket recycling |
| CN110171582A (en) * | 2019-06-03 | 2019-08-27 | 哈尔滨工业大学 | Spacecraft Recovery electromagnetic damping device |
| CN110185732A (en) * | 2019-06-03 | 2019-08-30 | 哈尔滨工业大学 | Spacecraft Recovery linear electromagnetic damping unit |
| CN110171582B (en) * | 2019-06-03 | 2021-11-19 | 哈尔滨工业大学 | Electromagnetic damping device for spacecraft recovery |
| CN110282160A (en) * | 2019-06-28 | 2019-09-27 | 中国科学院电工研究所 | Tubaeform electromagnetic type rocket landing recyclable device |
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Application publication date: 20180109 |