CN109764749A - Rocket weapon or transmitter emission system and method - Google Patents

Rocket weapon or transmitter emission system and method Download PDF

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Publication number
CN109764749A
CN109764749A CN201811491467.5A CN201811491467A CN109764749A CN 109764749 A CN109764749 A CN 109764749A CN 201811491467 A CN201811491467 A CN 201811491467A CN 109764749 A CN109764749 A CN 109764749A
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CN
China
Prior art keywords
platform
fixed
emission system
rocket
bearing diagonal
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Granted
Application number
CN201811491467.5A
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Chinese (zh)
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CN109764749B (en
Inventor
李盛
薛士明
蔺法鹏
刘斌
谢永刚
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Hubei Aerospace Craft Research Institute
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Hubei Aerospace Craft Research Institute
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Priority to CN201811491467.5A priority Critical patent/CN109764749B/en
Publication of CN109764749A publication Critical patent/CN109764749A/en
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Abstract

Rocket weapon or transmitter emission system characterized by comprising base platform, when use, which is fixed, to be set on the ground;Perpendicular platform is played, one end is rotatably fixed on the fixation position of base platform;Bearing diagonal platform, one end is rotatably connect with perpendicular platform is played, the other end is free end, wherein, the position far from fixed position of base platform is provided with locking structure, when rise perpendicular platform risen it is perpendicular turn to predetermined angular when, the free end of bearing diagonal platform is passed through to the locking structure fixation being arranged on base platform and is locked on base platform.The present invention completes box rocket projector design using pure mechanic structure scheme, solves the launch mission problem under low cost, fast pace and high reliability research condition, have the characteristics that easy to operate, inexpensive, high-intensitive, has widened the emission mode type of box rocket.

Description

Rocket weapon or transmitter emission system and method
Technical field
The invention belongs to rocket launching technologies, specifically design a kind of box rocket projector.
Background technique
The launch party of launch truck is mostly used for the anti-radiation pattern for pushing away spray projection device such as box rocket or guided missile Method, the functional full spies such as transmitting is reliable, mobility is high this is because traditional box launch truck has, heat preservation leveling Point, while the outstanding advantages that launch truck is high with high degree of automation and launch accuracy, therefore box launch truck is The conventional equipment that must be designed in rocket development process.
But funds are few, the period is short, the requirement of high reliablity since rocket launching system in recent years faces in development process It is further urgent, therefore the weapon system of some models, will be because of long in the launch truck lead time, or develop initial stage warp Take insufficient reason and not can guarantee timely output, influences the flight test launch mission of box rocket, and then it is vertical to influence model Item or contract competitive bidding.
Therefore, traditional box launch truck, which is unable to satisfy in reality, requires research and development production funds in need few, research and development week The requirement of phase short two while high reliablity.
Summary of the invention
The present invention is to carry out to solve the above-mentioned problems, and it is an object of the present invention to provide a kind of rocket weapon or transmitter transmitting System and method.
Relative to box launch truck, emission system provided by the invention uses pure mechanic structure scheme, solves low Launch mission problem under cost, fast pace and high reliability research condition, have the characteristics that it is easy to operate, inexpensive, high-intensitive, The emission mode type of box rocket is widened.
The present invention provides a kind of rocket weapon or transmitter emission systems characterized by comprising
Base platform, when use, which is fixed, to be set on the ground;
Perpendicular platform is played, one end is rotatably fixed on the fixation position of base platform;
Bearing diagonal platform, one end are rotatably connect with perpendicular platform is played, and the other end is free end,
Wherein, the position far from fixed position of base platform is provided with locking structure,
When rise perpendicular platform risen it is perpendicular turn to predetermined angular when, the free end of bearing diagonal platform is put down by setting in pedestal Locking structure fixation on platform is locked on base platform.
Rocket weapon or transmitter emission system provided by the invention, it is characterised in that:
Wherein, the one end for playing perpendicular platform is fixed pin shaft and is fixed on the fixation position of base platform.
Rocket weapon or transmitter emission system provided by the invention, it is characterised in that:
Wherein, one end of bearing diagonal platform is rotatably connect with perpendicular platform by pin shaft.
Rocket weapon or transmitter emission system provided by the invention, it is characterised in that:
Wherein, locking structure is the pin shaft hole being arranged on base platform,
When fixed, fixed pin shaft passes through pin shaft hole, and the free end of bearing diagonal platform is fastened on by fixed pin shaft At pin shaft hole.
Rocket weapon or transmitter emission system provided by the invention, it is characterised in that:
Wherein, the free end of bearing diagonal platform is provided with double threaded screw, by double threaded screw come so that on bearing diagonal platform Hole can and pin shaft hole to just for fixed pin shaft install.
Rocket weapon or transmitter emission system provided by the invention, which is characterized in that further include:
Fixed bracket, has been used to support perpendicular platform.
Rocket weapon or transmitter emission system provided by the invention, it is characterised in that:
Wherein, firm banking platform is welded using general profile U-typed channel steel and steel plate.
The present invention also provides a kind of rocket weapon or the launching techniques of transmitter emission system, which is characterized in that in use The rocket weapon or transmitter emission system stated are emitted, including following operation:
Fixed operation fixes base platform, has then installed perpendicular platform and bearing diagonal platform;
The rocket weapon that vanning is completed or transmitter are hung and are risen on perpendicular platform, and firing box is locked by lifting operation It is fixed;
Perpendicular operation is played, perpendicular platform will be played and erected to predetermined angular, and be locked on base platform by locking structure fixation;
It clears out a gathering place, rocket weapon or transmitter are in battery.
The launching technique of rocket weapon or transmitter emission system provided by the invention, can also have the following features:
Wherein, it in lifting operation, plays perpendicular platform and is mounted directly on hold-down support platform and is in by fixed pin shaft Horizontality simultaneously carries out Auxiliary support using fixed bracket.
The launching technique of rocket weapon or transmitter emission system provided by the invention, can also have the following features:
Wherein, when playing perpendicular operation, bearing diagonal platform one end has been fixed on perpendicular platform, and the other end directly falls in activity and pushes away Che Shang, so that movable trolley bears part inclination drag load.
The launching technique of rocket weapon or transmitter emission system provided by the invention, can also have the following features:
Wherein, it when playing perpendicular operation, is lifted by crane using two lifting appliances:
One head lifting lug for having connected perpendicular platform is lifted by crane;
The intermediate position of another connection bearing diagonal platform, which is lifted by crane and is attached to, pulls movable trolley close to base platform.
The action and effect of invention
Related rocket weapon or transmitter emission system according to the present invention, because of the base platform having, when use It is fixed and sets on the ground;Perpendicular platform is played, one end is rotatably fixed on the fixation position of base platform;Bearing diagonal is flat Platform, one end are rotatably connect with perpendicular platform is played, and the other end is free end, turn to predetermined angular when perpendicular platform is risen to erect When, the free end of bearing diagonal platform is passed through to the locking structure fixation being arranged on base platform and is locked on base platform, is led to It crosses simple three components and is attached combination, so that it may which a variety of launching elevations are set, and structure is simple.Thus with it is traditional box Launch truck compares, which has the advantage that
1, the present invention substantially reduces the lead time, can preferably guarantee development progress.
2, can assurance function require under the premise of, cost will greatly reduce, and task can guarantee to smoothly complete.
3, it is assembled simply in use process of the present invention, smoothly cooperating by 2 cranes of floor manager requirement can be completed whole Operation.
4, environmental suitability of the present invention is stronger, and a sets of plan is suitable for multinomial launch mission, meets range in the angle of departure and wants Under conditions of asking, can increase simple switching tooling can be realized the conversion of different box rocket launching tasks.
Detailed description of the invention
Fig. 1 has forecast perpendicular behaviour to finish when rocket weapon in the embodiment of the present invention or transmitter emission system lifting operation The structural schematic diagram of work;
Fig. 2 is that the structure of rocket weapon or transmitter emission system when having carried out perpendicular operation is shown in the embodiment of the present invention It is intended to;And
Fig. 3 be in the embodiment of the present invention rocket weapon or transmitter emission system rise perpendicular operation to it is vertical when structure show It is intended to.
Specific embodiment
It is real below in order to be easy to understand the technical means, the creative features, the aims and the efficiencies achieved by the present invention Example combination attached drawing is applied to be specifically addressed rocket weapon of the present invention or transmitter emission system and method.
Fig. 1 has forecast perpendicular behaviour to finish when rocket weapon in the embodiment of the present invention or transmitter emission system lifting operation The structural schematic diagram of work.
Fig. 2 is that the structure of rocket weapon or transmitter emission system when having carried out perpendicular operation is shown in the embodiment of the present invention It is intended to.
Fig. 3 be in the embodiment of the present invention rocket weapon or transmitter emission system rise perpendicular operation to it is vertical when structure show It is intended to.
Embodiment 1
As shown in Figure 1, rocket weapon or transmitter emission system, comprising:
Base platform 1, when use, which is fixed, to be set on the ground.
Perpendicular platform 2 is played, one end is rotatably fixed on the fixation position of base platform;
Bearing diagonal platform 3, one end are rotatably connect with perpendicular platform is played, and the other end is free end,
Wherein, the position far from fixed position of base platform is provided with locking structure,
When rise perpendicular platform risen it is perpendicular turn to predetermined angular when, the free end of bearing diagonal platform is put down by setting in pedestal Locking structure fixation on platform is locked on base platform.
Embodiment 2
On the basis of embodiment 1, as a kind of optimization, the one end for playing perpendicular platform is fixed pin shaft and is fixed on base platform Fixation position on;And/or
One end of bearing diagonal platform is rotatably connect with perpendicular platform by pin shaft;
And/or
Locking structure is the pin shaft hole being arranged on base platform,
When fixed, fixed pin shaft passes through pin shaft hole, and the free end of bearing diagonal platform is fastened on by fixed pin shaft 6 At pin shaft hole.
By using the scheme of fixed pin shaft, so that structure is simple, convenient for being quickly designed, when shortening design and manufacture Between.
Embodiment 3
On the basis of above-described embodiment 1-2, the free end of bearing diagonal platform is provided with double threaded screw, passes through double threaded screw To enable the hole on bearing diagonal platform and pin shaft hole to just installing for fixed pin shaft.
Embodiment 4
As one kind quickly manufacture it is preferred, firm banking platform using general profile U-typed channel steel and steel plate welding and At.
Embodiment 5
On the basis of above-described embodiment 1-4, below by taking the transmitting of box rocket J as an example, it is further provided a kind of reality The emission system of box rocket by verifying.
As shown in Figure 1, Figure 2 and Figure 3, the box rocket projector of the optimization mainly by base platform 1, perpendicular platform 2, Bearing diagonal platform 3, fixed bracket 4, movable trolley 5, fixed pin shaft 6 form.Box rocket J be product to be launched, crane D1 and Crane D2 is auxiliary tool.
Firm banking platform 1 uses general profile U-typed channel steel and steel plate welding fabrication, is the load base of emitter Plinth, base platform is after concrete launching level ground completes directive alignment using the fixed each supporting leg of expansion bolt
It plays perpendicular platform 2 and undertakes box rocket by the static load and dynamic load of horizontality to vertical state, and undertake flat with pedestal The installation of the structure of platform and firing box is fixed, and provides the suspender installation interface during erecting.It plays perpendicular platform 2 and passes through fixed pin Axis is mounted directly on hold-down support platform and in horizontality, carries out Auxiliary support using fixed bracket 4, plays perpendicular platform and hold Firing box and rocket are carried on a shoulder pole by the static load and dynamic load of horizontality to vertical state, and undertakes the structure with base platform and firing box Installation is fixed, and provides the suspender installation interface during erecting.
Bearing diagonal platform 3, which undertakes emitter, to be play a part of to fix locking after erecting launch angle.3 one end of bearing diagonal platform Fixed to rising on perpendicular platform, the other end is directly fallen on movable trolley 5, bears inclination drag load.
Fixed bracket 4 and movable trolley 5 undertake emitter and act Auxiliary support during erecting.
Embodiment 6
The present embodiment provides the launching techniques of a kind of above-mentioned rocket weapon or transmitter emission system, use embodiment 1- Rocket weapon or transmitter emission system in 5 are emitted, including following operation:
Fixed operation fixes base platform, has then installed perpendicular platform and bearing diagonal platform;
The rocket weapon that vanning is completed or transmitter are hung and are risen on perpendicular platform, and firing box is locked by lifting operation It is fixed;
Perpendicular operation is played, perpendicular platform will be played and erected to predetermined angular, and be locked on base platform by locking structure fixation;
It clears out a gathering place, rocket weapon or transmitter are in battery.
Embodiment 7
On the basis of embodiment 6, as a kind of optimization, in lifting operation, it is direct by fixed pin shaft to play perpendicular platform It is installed on hold-down support platform and carries out Auxiliary support in horizontality, and using fixed bracket 4.
Embodiment 8
On the basis of embodiment 6-7, as a kind of optimization, when playing perpendicular operation, bearing diagonal platform one end is fixed to On perpendicular platform, the other end is directly fallen on movable trolley, so that movable trolley bears part inclination drag load.
Embodiment 9
On the basis of embodiment 6-8, risen when playing perpendicular operation using two lifting appliances as a kind of optimization Hang: a head lifting lug for having connected perpendicular platform is lifted by crane;It is lifted by crane at the intermediate position of another connection bearing diagonal platform And it is attached to and pulls movable trolley close to base platform.
Embodiment 10
On the basis of above-described embodiment 6-9, below by taking the transmitting of box rocket J as an example, it is further provided a kind of reality The launching technique of box rocket by verifying.
.
Fixed operation.Firm banking platform 1 is consolidated after concrete launching level ground completes basic leveling with expansion bolt It is fixed.
Lifting operation.It plays perpendicular platform 2 and horizontality is mounted directly on hold-down support platform and be in by fixed pin shaft, Auxiliary support is carried out using fixed bracket 4, perpendicular platform is played and undertakes firing box and rocket by the static load of horizontality to vertical state And dynamic load, and undertake to install with the structure of base platform and firing box and fix, and the suspender installation provided during erecting connects Mouthful.
As illustrated in fig. 1 and 2, the box rocket that vanning is completed is hung on perpendicular platform 2 by crane and suspender, using special Firing box is locked with locking pin.
Play perpendicular operation.3 one end of bearing diagonal platform has been fixed on perpendicular platform, and the other end is directly fallen on movable trolley 5, is held By inclination drag load.
Perpendicular platform 2 will be played using 2 cranes and suspender rise erect to predetermined angular:
The head lifting lug that one crane D1 has connected perpendicular platform is lifted by crane;
The intermediate position of another crane D2 connection bearing diagonal platform, which is lifted by crane and is attached to, pulls movable trolley the bottom of close to Seat platform.
Rise erect to predetermined angular after bearing diagonal platform 3 is locked to base platform 1 with fixed pin shaft 6 pin hole at, it is right If any a small amount of deviation during hole, double threaded screw in fine-tuning bearing diagonal platform 3 guarantees mounting hole to just.
Fixed bracket 4 is withdrawn from after finishing.
It clears out a gathering place.It finally removes suspender, withdraw crane and movable trolley 5, box rocket is in battery.
The action and effect of embodiment
The rocket weapon according to involved in embodiment or transmitter emission system, because of the base platform having, when use It is fixed and sets on the ground;Perpendicular platform is played, one end is rotatably fixed on the fixation position of base platform;Bearing diagonal is flat Platform, one end are rotatably connect with perpendicular platform is played, and the other end is free end, turn to predetermined angular when perpendicular platform is risen to erect When, the free end of bearing diagonal platform is passed through to the locking structure fixation being arranged on base platform and is locked on base platform, is led to It crosses simple three components and is attached combination, so that it may which a variety of launching elevations are set, and structure is simple.Thus with it is traditional box Launch truck compares, and the scheme that embodiment provides has the advantage that
1, the lead time is substantially reduced, can preferably guarantee development progress.
2, can assurance function require under the premise of, cost will greatly reduce, and task can guarantee to smoothly complete.
3, it is assembled simply in use process, smoothly cooperating by 2 cranes of floor manager requirement can be completed all operationss.
4, environmental suitability is stronger, and a sets of plan is suitable for multinomial launch mission, meets the item of area requirement in the angle of departure Under part, can increase simple switching tooling can be realized the conversion of different box rocket launching tasks.
Above embodiment is preferred case of the invention, the protection scope being not intended to limit the invention.

Claims (10)

1. a kind of rocket weapon or transmitter emission system characterized by comprising
Base platform, when use, which is fixed, to be set on the ground;
Perpendicular platform is played, one end is rotatably fixed on the fixation position of the base platform;
Bearing diagonal platform, one end are rotatably connect with described perpendicular platform, and the other end is free end,
Wherein, the position far from the fixed position of the base platform is provided with locking structure,
When described perpendicular platform risen it is perpendicular turn to predetermined angular when, by the free end of the bearing diagonal platform by being arranged in institute The locking structure fixation stated on base platform is locked on the base platform.
2. rocket weapon according to claim 1 or transmitter emission system, it is characterised in that:
Wherein, one end of described perpendicular platform is fixed pin shaft and is fixed on the fixation position of the base platform.
3. rocket weapon according to claim 1 or transmitter emission system, it is characterised in that:
Wherein, one end of the bearing diagonal platform is rotatably connect with described perpendicular platform by pin shaft.
4. rocket weapon according to claim 1 or transmitter emission system, it is characterised in that:
Wherein, the locking structure is the pin shaft hole being arranged on base platform,
When fixed, fixed pin shaft passes through the pin shaft hole, and the free end of the bearing diagonal platform is connected admittedly by fixed pin shaft It is scheduled at the pin shaft hole.
5. rocket weapon according to claim 4 or transmitter emission system, it is characterised in that:
Wherein, the free end of the bearing diagonal platform is provided with double threaded screw, by double threaded screw come so that the bearing diagonal is flat Hole on platform can be with the pin shaft hole to just for fixed pin shaft installation.
6. rocket weapon according to claim 4 or transmitter emission system, it is characterised in that:
Wherein, the firm banking platform is welded using general profile U-typed channel steel and steel plate.
7. the launching technique of a kind of rocket weapon or transmitter emission system, which is characterized in that using any in claim 1-6 One rocket weapon or transmitter emission system is emitted, including following operation:
Fixed operation fixes the base platform, and then installation is described plays perpendicular platform and the bearing diagonal platform;
The rocket weapon that vanning is completed or transmitter are hung on described perpendicular platform, and firing box are locked by lifting operation It is fixed;
Perpendicular operation is played, described perpendicular platform is risen and is erected to predetermined angular, and is locked at the pedestal by the way that locking structure is fixed and puts down On platform;
It clears out a gathering place, the rocket weapon or transmitter are in battery.
8. the launching technique of rocket weapon according to claim 7 or transmitter emission system, it is characterised in that:
Wherein, in lifting operation, described perpendicular platform is mounted directly on the hold-down support platform simultaneously by fixed pin shaft Auxiliary support is carried out in horizontality and using fixed bracket.
9. the launching technique of rocket weapon according to claim 7 or transmitter emission system, it is characterised in that:
Wherein, when playing perpendicular operation, bearing diagonal platform one end is risen on perpendicular platform fixed to described, and the other end directly falls in work On dynamic cart, so that movable trolley bears part inclination drag load.
10. the launching technique of rocket weapon according to claim 9 or transmitter emission system, it is characterised in that:
Wherein, it when playing perpendicular operation, is lifted by crane using two lifting appliances:
One connection head lifting lug for playing perpendicular platform is lifted by crane;
The intermediate position of another connection bearing diagonal platform, which is lifted by crane and is attached to, pulls the movable trolley close to described Base platform.
CN201811491467.5A 2018-12-07 2018-12-07 Method for launching a rocket weapon or launcher launching system Active CN109764749B (en)

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110274520A (en) * 2019-06-13 2019-09-24 蓝箭航天空间科技股份有限公司 Perpendicular device and rocket launching auxiliary system are played for rocket launching
CN111256533A (en) * 2020-02-24 2020-06-09 北京中科宇航技术有限公司 Vertical rocker arm
CN111928734A (en) * 2020-08-28 2020-11-13 湖北航天技术研究院总体设计所 Carrier launching module and carrier launching method
CN114543591A (en) * 2022-03-08 2022-05-27 鲁东大学 Marine rocket transportation and launching method
CN114705080A (en) * 2022-02-11 2022-07-05 广东空天科技研究院 Deformable and recyclable rocket aircraft aerial launching system
CN114812272A (en) * 2022-06-28 2022-07-29 东方空间技术(北京)有限公司 Rocket erecting device and rocket transferring erecting system

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6186039B1 (en) * 1998-02-25 2001-02-13 Kistler Aerospace Corporation Spacecraft launch system and method
CN2911601Y (en) * 2006-05-17 2007-06-13 山西北方惠丰机电有限公司 Vehicle-mounted launching system
CN101654151A (en) * 2009-09-02 2010-02-24 中兵光电科技股份有限公司 Supporting mechanism applied unmanned aerial vehicle launching system
CN202101605U (en) * 2011-06-03 2012-01-04 江西钢丝厂 Vehicle-mounted electric launching rack capable of moving horizontally and automatically
RU2477247C1 (en) * 2011-09-22 2013-03-10 Публичное акционерное общество "ДНЕПРОТЯЖМАШ" Device for lifting carrier rocket mounter and retaining it vertically at launch pad
CN106197146A (en) * 2016-08-12 2016-12-07 清华大学 A kind of rocket model and the adjustable rocket launch platform of attitude
CN206056393U (en) * 2016-06-29 2017-03-29 贵州航天天马机电科技有限公司 A kind of rocket plays perpendicular device and stably plays perpendicular and quick rewind system
CN108562189A (en) * 2018-03-20 2018-09-21 西安航天动力技术研究所 A kind of sounding rocket emitter

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6186039B1 (en) * 1998-02-25 2001-02-13 Kistler Aerospace Corporation Spacecraft launch system and method
CN2911601Y (en) * 2006-05-17 2007-06-13 山西北方惠丰机电有限公司 Vehicle-mounted launching system
CN101654151A (en) * 2009-09-02 2010-02-24 中兵光电科技股份有限公司 Supporting mechanism applied unmanned aerial vehicle launching system
CN202101605U (en) * 2011-06-03 2012-01-04 江西钢丝厂 Vehicle-mounted electric launching rack capable of moving horizontally and automatically
RU2477247C1 (en) * 2011-09-22 2013-03-10 Публичное акционерное общество "ДНЕПРОТЯЖМАШ" Device for lifting carrier rocket mounter and retaining it vertically at launch pad
CN206056393U (en) * 2016-06-29 2017-03-29 贵州航天天马机电科技有限公司 A kind of rocket plays perpendicular device and stably plays perpendicular and quick rewind system
CN106197146A (en) * 2016-08-12 2016-12-07 清华大学 A kind of rocket model and the adjustable rocket launch platform of attitude
CN108562189A (en) * 2018-03-20 2018-09-21 西安航天动力技术研究所 A kind of sounding rocket emitter

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110274520A (en) * 2019-06-13 2019-09-24 蓝箭航天空间科技股份有限公司 Perpendicular device and rocket launching auxiliary system are played for rocket launching
CN110274520B (en) * 2019-06-13 2020-09-01 蓝箭航天空间科技股份有限公司 Erecting device for rocket launching and rocket launching auxiliary system
CN111256533A (en) * 2020-02-24 2020-06-09 北京中科宇航技术有限公司 Vertical rocker arm
CN111256533B (en) * 2020-02-24 2022-02-01 北京中科宇航技术有限公司 Vertical rocker arm
CN111928734A (en) * 2020-08-28 2020-11-13 湖北航天技术研究院总体设计所 Carrier launching module and carrier launching method
CN114705080A (en) * 2022-02-11 2022-07-05 广东空天科技研究院 Deformable and recyclable rocket aircraft aerial launching system
CN114705080B (en) * 2022-02-11 2023-09-29 广东空天科技研究院 Deformable and recyclable rocket type aircraft air launching system
CN114543591A (en) * 2022-03-08 2022-05-27 鲁东大学 Marine rocket transportation and launching method
CN114543591B (en) * 2022-03-08 2023-09-26 鲁东大学 Marine rocket transporting and launching method
CN114812272A (en) * 2022-06-28 2022-07-29 东方空间技术(北京)有限公司 Rocket erecting device and rocket transferring erecting system
CN114812272B (en) * 2022-06-28 2022-09-02 东方空间技术(北京)有限公司 Rocket erecting device and rocket transferring erecting system

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