CN215177250U

CN215177250U - Rocket launching platform

Info

Publication number: CN215177250U
Application number: CN202121214865.XU
Authority: CN
Inventors: 邢春雷; 布向伟; 王永刚; 魏凯; 郝丁; 王亚男; 黄亚军; 吴考
Original assignee: Dongfang Space Technology Shandong Co Ltd
Current assignee: Dongfang Space Technology Shandong Co Ltd
Priority date: 2021-06-01
Filing date: 2021-06-01
Publication date: 2021-12-14
Anticipated expiration: 2031-06-01

Abstract

The utility model provides a rocket launching platform, this rocket launching platform for transport and launch the rocket, rocket launching platform includes: a load-bearing hull; the supporting platform is arranged at one end of the bearing ship body, extends towards the direction far away from the bearing ship body, and at least part of the supporting platform is in a suspended state; the launching platform is movably arranged on the supporting platform, an rocket body bracket is arranged on the launching platform, and the rocket is vertically placed on the rocket body bracket. Through the technical scheme provided by the application, the problems of complex operation and long time of the marine rocket launcher in the related technology can be solved.

Description

Rocket launching platform

Technical Field

The utility model relates to a space flight ground support equipment technical field particularly, relates to a rocket launching platform.

Background

The marine launching rocket has the characteristics of strong flexibility, good task adaptability, excellent launching economy and the like, can flexibly select launching points and landing areas, and meets the launching requirements of various tracks.

Meanwhile, marine launching also needs to be adjusted, such as marine transfer, preparation before launching and the like are adapted to differences from land, for example, the long symbol 11 in China is horizontally transferred through the sea, test preparation before launching is carried out in a launching sea area, and then vertical launching is carried out. Therefore, the problems of complex operation and long time of the marine rocket launcher exist in the related art.

SUMMERY OF THE UTILITY MODEL

The utility model provides a rocket launching platform to solve the problem that the marine launch rocket operation among the correlation technique is complicated, long-term.

The utility model provides a rocket launching platform for transport and launch rocket, rocket launching platform includes: a load-bearing hull; the supporting platform is arranged at one end of the bearing ship body, extends towards the direction far away from the bearing ship body, and at least part of the supporting platform is in a suspended state; the launching platform is movably arranged on the supporting platform, an rocket body bracket is arranged on the launching platform, and the rocket is vertically placed on the rocket body bracket.

Further, the rocket body bracket comprises a base body and a plurality of fixing units which are connected with each other, the rocket is vertically placed on the base body, and the lower end of the rocket is connected with the fixing units.

Further, the fixing unit is of an annular structure, and the axis of the fixing unit extends in the vertical direction; and/or, the rocket body bracket still includes a plurality of strengthening ribs, and the equal interval in periphery of each fixed unit is provided with a plurality of strengthening ribs, and the one end and the fixed unit of strengthening rib are connected, and the other end and the pedestal of strengthening rib are connected, and the strengthening rib slope sets up.

Further, the rocket launching platform further comprises a wave compensation mechanism, and the wave compensation mechanism is arranged between the bearing ship body and the supporting platform.

Furthermore, a first rail is arranged on the supporting platform, the first rail extends along the length direction of the supporting platform, and the launching platform is movably arranged on the first rail.

Furthermore, the rocket launching platform also comprises a service tower, a second track is arranged on the supporting platform, the second track extends along the length direction of the supporting platform, and the service tower is movably arranged on the second track; the first track and the second track are arranged at intervals, a supporting boss is arranged between the first track and the second track, and the service tower and the launching platform are supported on the supporting boss.

Furthermore, the rocket launching platform also comprises a flow director, the part of the supporting platform in a suspended state is provided with a flame discharge hole, the flow director is positioned below the flame discharge hole, and the flow director floats on the sea surface.

Further, the flow guide comprises a main body and a flow guide part, the flow guide part is arranged on the upper surface of the main body, the flow guide part extends from one side of the main body to the other side of the main body, the size of the cross section of the flow guide part is gradually reduced in the direction from bottom to top, and the side wall of the flow guide part is a curved surface or an inclined surface.

Further, the rocket launching platform also comprises a locking structure, and the locking structure is arranged between the launching platform and the supporting platform.

Further, the launching platform includes rack and drive division, and the rocket body bracket sets up on the rack, and drive division includes a plurality of drive unit, and a plurality of drive unit intervals set up the lower extreme at the rack.

Use the technical scheme of the utility model, when utilizing rocket launching platform transportation and launch rocket, at first will bear the hull and open the pier and make supporting platform's tip that is in unsettled state align with the pier, then be connected supporting platform and pier, bear the launching pad and catch fire the rocket and remove the preset position on the supporting platform. Because the rocket body bracket is arranged on the launching platform, the rocket can be vertically placed on the rocket body bracket, the loading ship body is driven to the launching sea area without erecting the rocket, and the rocket can be directly launched. By adopting the structure, the rocket is vertically transported on the sea and launched on the sea, the time of assembling and butting on the sea is saved, the preparation flow before launching is simplified, the operation of launching the rocket on the sea can be simplified, and the time of launching the rocket on the sea is shortened.

Drawings

The accompanying drawings, which form a part of the present application, are included to provide a further understanding of the invention, and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention and together with the description serve to explain the invention and not to limit the invention. In the drawings:

fig. 1 shows a schematic structural diagram of a rocket launch platform provided in accordance with an embodiment of the present invention;

FIG. 2 illustrates a partial enlarged view of a rocket launch platform provided in accordance with an embodiment of the present invention;

FIG. 3 shows a schematic diagram of the transmitting station of FIG. 1;

fig. 4 shows a schematic view of the fluid director in fig. 1.

Wherein the figures include the following reference numerals:

10. a load-bearing hull; 20. a support platform; 21. a first track; 22. a second track; 23. supporting the boss; 24. a flame discharge hole; 30. a launch pad; 31. an arrow body bracket; 311. a base body; 312. a fixing unit; 313. reinforcing ribs; 32. a rack; 33. a drive section; 331. a drive unit; 40. a service tower; 50. a fluid director; 51. a main body; 52. a flow guide part.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. The following description of at least one exemplary embodiment is merely illustrative in nature and is in no way intended to limit the invention, its application, or uses. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative efforts belong to the protection scope of the present invention.

As shown in fig. 1 to 4, embodiments of the present invention provide a rocket launching platform for transporting and launching rockets, comprising a load-bearing hull 10, a support platform 20 and a launch pad 30. The support platform 20 is disposed at one end of the load-bearing hull 10, the support platform 20 extends away from the load-bearing hull 10, and at least a portion of the support platform 20 is suspended. Launch pad 30 is movably disposed on support platform 20, and launch pad 30 is provided with rocket body bracket 31, and the rocket is placed on rocket body bracket 31 vertically.

With the rocket launching platform provided in this embodiment, when transporting and launching a rocket by using the rocket launching platform, the loading hull 10 is first opened to the dock so that the end of the supporting platform 20 in a suspended state is aligned with the dock, then the supporting platform 20 is connected to the dock, and the launching platform 30 is moved to a preset position on the supporting platform 20 for loading the rocket. Since the rocket body brackets 31 are arranged on the launching platform 30, the rocket can be vertically placed on the rocket body brackets 31, and the rocket can be directly launched without erecting the rocket after the bearing ship body 10 is driven to the launching sea area. By adopting the structure, the rocket is vertically transported on the sea and launched on the sea, the time of assembling and butting on the sea is saved, the preparation flow before launching is simplified, the operation of launching the rocket on the sea can be simplified, and the time of launching the rocket on the sea is shortened.

It should be noted that at least a part of the supporting platforms 20 are in a suspended state, and the supporting platforms include two structures, the first structure is that a part of the supporting platforms 20 are in a suspended state, and the other part of the supporting platforms 20 are fixed on the carrying hull 10; the second configuration is where all the support platforms 20 are in a suspended state, and the support platforms 20 can be connected to the load-bearing hull 10 by connecting members such as connecting rods.

In the present embodiment, the supporting platform 20 is of a first structure, that is, a part of the supporting platform 20 is in a suspended state, and another part of the supporting platform 20 is fixed on the carrying hull 10. With the above structure, the support platform 20 has sufficient connection strength with the load-bearing hull 10.

As shown in fig. 3, the rocket body holder 31 includes a holder body 311 and a plurality of fixing units 312 which are connected to each other, and the rocket is vertically placed on the holder body 311, and the lower end of the rocket is connected to the fixing units 312. Utilize pedestal 311 to support the rocket, utilize a plurality of fixed unit 312 to fix the rocket simultaneously, guarantee the steadiness of rocket.

In the present embodiment, the fixing unit 312 has a ring structure, and an axis of the fixing unit 312 extends in a vertical direction. The fixing unit 312 having a ring structure can achieve a good fixing effect, and ensure stability in the process of vertically transporting the rocket.

In order to further enhance the fixing effect and the structural stability, the arrow body bracket 31 further includes a plurality of reinforcing ribs 313, a plurality of reinforcing ribs 313 are arranged at intervals on the periphery of each fixing unit 312, one end of each reinforcing rib 313 is connected with the fixing unit 312, the other end of each reinforcing rib 313 is connected with the base body 311, and the reinforcing ribs 313 are arranged in an inclined manner.

In this embodiment, the rocket launch platform further comprises a heave compensation mechanism disposed between the load-bearing hull 10 and the support platform 20. Utilize the wave compensation mechanism to compensate the wave fluctuation on the sea, guarantee that supporting platform 20 can not appear great rocking, and then guarantee that supporting platform 20 and launch pad 30 can be in relatively steady state in transportation and launch process.

In this embodiment, the heave compensation mechanism comprises a detection part, a control part and an adjustment part, wherein the control part is electrically connected with the detection part and the adjustment part, the detection part detects the state parameters of the bearing hull 10 and the supporting platform 20, the control part controls the adjustment part to work according to the state parameters detected by the detection part, and the adjustment part adjusts the position of the supporting platform 20 so as to keep the supporting platform 20 stable.

Specifically, the detection section includes a position sensor for detecting the position of the support platform 20 with respect to the load-bearing hull 10, and a level sensor for detecting the level state of the support platform 20. The adjusting part comprises a push rod assembly, the push rod assembly comprises a plurality of mutually matched push rod units, the push rod units are used for driving the supporting platform 20 to move relative to the bearing ship body 10, and therefore the supporting platform 20 is guaranteed to be stable.

As shown in fig. 2, a first rail 21 is disposed on the supporting platform 20, the first rail 21 extends along the length direction of the supporting platform 20, and the launching platform 30 is movably disposed on the first rail 21. By providing the first rail 21, on the one hand, the friction force when the launching platform 30 moves can be reduced, and on the other hand, a predetermined path can be provided for the launching platform 30 by using the first rail 21, so that the launching platform 30 can move along the predetermined path.

As shown in fig. 2, the rocket launching platform further comprises a service tower 40, the support platform 20 is provided with a second rail 22, the second rail 22 extends along the length direction of the support platform 20, and the service tower 40 is movably arranged on the second rail 22. Likewise, the use of the second track 22 can, on the one hand, reduce friction when the service tower 40 is moving and, on the other hand, can provide a predetermined path for the service tower 40 using the second track 22 to ensure that the service tower 40 moves along the predetermined path.

The service tower 40 is of a steel frame structure, and corresponding closed or open working platforms are arranged on the service tower 40 at different heights of the carrier rocket, so that workers can approach the carrier rocket conveniently.

In this embodiment, the first rail 21 and the second rail 22 are arranged at intervals, the supporting boss 23 is arranged between the first rail 21 and the second rail 22, and the service tower 40 and the launching platform 30 are supported on the supporting boss 23, so that the structural stability is ensured.

Specifically, the support bosses 23 are elongated bosses, and the support bosses 23 extend along the length direction of the support platform 20. The bottom of the service tower 40 has a stepped structure including a vertical section and a horizontal section connected to each other, the horizontal section being located above the support boss 23, the vertical section extending downward and being located outside the support platform 20, and an end of the vertical section being slidably supported on the second rail 22. The emission stage 30 has protrusions extending outward at both sides thereof, and the protrusions are located above the support bosses 23. In the present embodiment, the second rail 22 is located outside the first rail 21.

As shown in fig. 2 and 4, the rocket launching platform further comprises a deflector 50, the portion of the supporting platform 20 in a suspended state is provided with the exhaust ports 24, the deflector 50 is located below the exhaust ports 24, and the deflector 50 floats on the sea surface. When the rocket is launched, the flames at the bottom of the rocket can be discharged through the flame discharge holes 24, and the flames are guided by the deflectors 50. Through arranging the exhaust ports 24 at the part of the supporting platform 20 in a suspended state, the rocket does not need to be moved after being transported to a launching position, so that the launching steps can be simplified, and the launching efficiency can be improved.

Specifically, the flow guide 50 includes a main body 51 and a flow guide part 52, the flow guide part 52 is disposed on the upper surface of the main body 51, the flow guide part 52 extends from one side of the main body 51 to the other side of the main body 51, the cross-sectional size of the flow guide part 52 is gradually reduced in the direction from bottom to top, and the side wall of the flow guide part 52 is a curved surface or an inclined surface. With the above structure of the flow guide 50, when the flame passes through the flow guide part 52, a good flow guide effect can be achieved by using the flow guide part 52.

In this embodiment, the side wall of the guiding portion 52 is an inclined surface, so that the path of the flame moving along the side wall of the guiding portion 52 is smoother, and the guiding effect is better.

To secure the launch pad 30, the rocket launch platform further includes a locking structure disposed between the launch pad 30 and the support platform 20. The locking structure includes, but is not limited to, a structure of fastening, a structure of fixing a pin, and only the locking structure can be used to fix the launching platform 30.

In this embodiment, the locking structure is a structure connected by fasteners, and the launching platform 30 is locked on the supporting platform 20 by the fasteners, so as to ensure the stability of the launching platform 30 during transportation and launching.

As shown in fig. 3, the launching stage 30 includes a stage 32 and a driving part 33, the arrow body holder 31 is disposed on the stage 32, the driving part 33 includes a plurality of driving units 331, and the plurality of driving units 331 are disposed at intervals at a lower end of the stage 32. The plurality of driving units 331 are used for driving the launching platform 30 to move simultaneously, so that the stability of the launching platform 30 in moving can be ensured.

Specifically, the driving unit 331 includes a plurality of wheel sets and a driving member, and the driving member is drivingly connected to the wheel sets.

It should be noted that the load-bearing hull 10 includes, but is not limited to, a ship and an offshore work platform.

The fuel types of rockets include both solid and liquid, and in the case of liquid fuels for the rocket, the liquid fuel oxidizer and fuel are stored separately prior to launching the liquid fuel rocket. After the rocket reaches the launch point, the oxidizer and fuel are mixed.

Wherein the rocket launch platform further comprises a filling hull, the load-bearing hull 10 being used for transporting and launching the rocket. One of the load carrying hull 10 and the filling hull has an oxidant tank and the other of the load carrying hull 10 and the filling hull has a fuel tank. The oxidizer and the fuel are separately stored on two independent ship hulls, so that the possibility of contact between the oxidizer and the fuel does not exist in the process of transporting the rocket from land to a launching point at sea, and the safety of the transportation of the oxidizer and the fuel can be further ensured.

In particular, the oxidizer tank is provided at one end of the load-bearing hull 10, the oxidizer tank not taking up too much space of the load-bearing hull 10.

Wherein the launching station 30 and the oxidizer tank are located at the two ends of the load-bearing hull 10, respectively. The distance between the oxidizer tank and the launching platform 30 is far, and the distance between the oxidizer tank and the rocket is also far in the process of transporting and launching the rocket due to the fact that the rocket is arranged on the launching platform 30, and safety can be further improved. The fuel storage tank is arranged at the bow of the filling ship body, so that fuel can be conveniently filled into the fuel storage tank, and the fuel in the fuel storage tank can be conveniently filled into the rocket.

Specifically, the fuel storage tank is provided with an infusion pipeline, the rocket is provided with a filling port, and the infusion pipeline fills fuel into the rocket through the filling port, so that the fuel filling efficiency is ensured.

To facilitate understanding of the rocket launching platform provided in this embodiment, the following description is made in conjunction with a method for using the rocket launching platform, where the method for using the rocket launching platform includes:

step S100, mooring the bearing ship 10 to an ashore, moving the launching platform 30 to the ashore through the supporting platform 20, and leveling the rocket body bracket 31 on the launching platform 30;

step S200, hoisting the whole arrow assembly, and vertically fixing the whole arrow assembly on the arrow body bracket 31;

step S300, completing the vertical test work of the whole rocket assembly on the shore, and moving the launching platform 30 back to the bearing ship body 10;

step S400, driving the bearing ship body 10 away from the wharf and towards a launching sea area, and carrying out test work before launching after reaching the launching sea area;

step S500, the launching platform 30 is moved to the suspended portion of the supporting platform 20, and finally the launching task is completed.

In step S100, the load-bearing hull 10 is moored ashore, specifically, the end of the load-bearing hull 10 is moored ashore, so that the support platform 20 is articulated with the quay.

Step S300 further includes: and (4) translating the service tower to the arrow body, and carrying out heat preservation, moisture prevention and auxiliary support in the driving process on the arrow body.

In step S400, if the rocket is a liquid rocket, the test is performed after the rocket is fueled, and the test is launched after the test is passed.

In step S500, after the launching platform 30 is moved to the portion of the supporting platform 20 in the suspended state, the deflector is placed right under the flame discharge hole, and finally the launching task is completed.

In this embodiment, the method for using the rocket launching platform further includes: step S600, the launching platform 30 slides to the central position of the ship, the fluid director is retracted, and the bearing ship body 10 drives back to the wharf.

In this embodiment, the whole rocket assembly includes a rocket, a booster and a satellite assembly, and step S200 specifically includes:

step S210, vertically hoisting the rocket to the rocket body bracket 31, adjusting the rocket body bracket to be vertical, and then fixing the rocket body bracket;

step S220, hoisting the booster, and vertically assembling the booster and the rocket;

and step S230, hoisting the satellite assembly, completing satellite-rocket butt joint, and further completing vertical final assembly of the whole rocket assembly.

In step S210, the rocket is vertically hoisted to the rocket body bracket 31, and is fixed after being vertically adjusted, specifically including: after the rocket is adjusted to be vertical, the rocket is fixed on the rocket body bracket through the windproof pull rod.

In this embodiment, the rocket is a core-stage rocket, and the satellite assembly includes a core-stage upper stage and a satellite cap assembly.

With the rocket launching platform provided in this embodiment, the load-bearing hull 10 is driven to quay so that the tracks on the support platform 20 are aligned with the tracks on the quay, the support platform 20 is hingedly connected to the quay, the service tower 40 is driven from the quay through the support platform 20 to the load-bearing hull 10, finally the launch station 30 is driven to the load-bearing hull 10 to launch the ship to the launching sea to complete the launching task. By carrying out offshore vertical transportation and offshore launching on the rocket, the time for offshore assembly and butt joint is saved, the preparation process before launching is simplified, the operation for launching the rocket on the sea can be further simplified, and the time for launching the rocket on the sea is shortened.

It is noted that the terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of example embodiments according to the present application. As used herein, the singular forms "a", "an" and "the" are intended to include the plural forms as well, and it should be understood that when the terms "comprises" and/or "comprising" are used in this specification, they specify the presence of stated features, steps, operations, devices, components, and/or combinations thereof, unless the context clearly indicates otherwise.

Unless specifically stated otherwise, the relative arrangement of the components and steps, the numerical expressions, and numerical values set forth in these embodiments do not limit the scope of the present invention. Meanwhile, it should be understood that the sizes of the respective portions shown in the drawings are not drawn in an actual proportional relationship for the convenience of description. Techniques, methods, and apparatus known to those of ordinary skill in the relevant art may not be discussed in detail but are intended to be part of the specification where appropriate. In all examples shown and discussed herein, any particular value should be construed as merely illustrative, and not limiting. Thus, other examples of the exemplary embodiments may have different values. It should be noted that: like reference numbers and letters refer to like items in the following figures, and thus, once an item is defined in one figure, further discussion thereof is not required in subsequent figures.

In the description of the present invention, it should be understood that the orientation or positional relationship indicated by the orientation words such as "front, back, up, down, left, right", "horizontal, vertical, horizontal" and "top, bottom" etc. are usually based on the orientation or positional relationship shown in the drawings, and are only for convenience of description and simplification of description, and in the case of not making a contrary explanation, these orientation words do not indicate and imply that the device or element referred to must have a specific orientation or be constructed and operated in a specific orientation, and therefore, should not be interpreted as limiting the scope of the present invention; the terms "inner and outer" refer to the inner and outer relative to the profile of the respective component itself.

Spatially relative terms, such as "above … …," "above … …," "above … …," "above," and the like, may be used herein for ease of description to describe one device or feature's spatial relationship to another device or feature as illustrated in the figures. It will be understood that the spatially relative terms are intended to encompass different orientations of the device in use or operation in addition to the orientation depicted in the figures. For example, if a device in the figures is turned over, devices described as "above" or "on" other devices or configurations would then be oriented "below" or "under" the other devices or configurations. Thus, the exemplary term "above … …" can include both an orientation of "above … …" and "below … …". The device may be otherwise variously oriented (rotated 90 degrees or at other orientations) and the spatially relative descriptors used herein interpreted accordingly.

It should be noted that the terms "first", "second", and the like are used to define the components, and are only used for convenience of distinguishing the corresponding components, and if not stated otherwise, the terms have no special meaning, and therefore, the scope of the present invention should not be construed as being limited.

The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention, and various modifications and changes may be made by those skilled in the art. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.

Claims

1. A rocket launch platform for transporting and launching rockets, said rocket launch platform comprising:

a load-bearing hull (10);

the supporting platform (20) is arranged at one end of the bearing ship body (10), the supporting platform (20) extends towards the direction far away from the bearing ship body (10), and at least part of the supporting platform (20) is in a suspended state;

the rocket launching device comprises a launching platform (30) movably arranged on the supporting platform (20), wherein rocket body brackets (31) are arranged on the launching platform (30), and the rocket is vertically placed on the rocket body brackets (31).

2. A rocket launch platform according to claim 1, characterized in that said rocket body receptacle (31) comprises an interconnected seat (311) and a plurality of fixed units (312), said rocket being placed vertically on said seat (311), the lower end of said rocket being connected to said fixed units (312).

3. A rocket launch platform according to claim 2,

the fixing unit (312) is of an annular structure, and the axis of the fixing unit (312) extends along the vertical direction; and/or the presence of a gas in the gas,

the rocket body bracket (31) still includes a plurality of strengthening ribs (313), each the equal interval in periphery of fixed unit (312) is provided with a plurality ofly strengthening rib (313), the one end of strengthening rib (313) with fixed unit (312) are connected, the other end of strengthening rib (313) with pedestal (311) are connected, just strengthening rib (313) slope sets up.

4. A rocket launch platform according to claim 1, characterized in that it further comprises a heave compensation mechanism, which is arranged between said load-bearing hull (10) and said support platform (20).

5. A rocket launch platform according to claim 1, characterized in that said support platform (20) is provided with a first rail (21), said first rail (21) extending along the length direction of said support platform (20), said launch pad (30) being movably arranged on said first rail (21).

6. A rocket launch platform according to claim 5,

the rocket launching platform further comprises a service tower (40), a second rail (22) is arranged on the supporting platform (20), the second rail (22) extends along the length direction of the supporting platform (20), and the service tower (40) is movably arranged on the second rail (22);

the first rail (21) and the second rail (22) are arranged at intervals, a supporting boss (23) is arranged between the first rail (21) and the second rail (22), and the service tower (40) and the launching platform (30) are supported on the supporting boss (23).

7. A rocket launch platform according to claim 1, characterized in that said rocket launch platform further comprises a deflector (50), the portion of said support platform (20) in suspension being provided with a fire vent (24), said deflector (50) being located below said fire vent (24), said deflector (50) floating on the sea surface.

8. A rocket launch platform according to claim 7, characterized in that said deflector (50) comprises a main body (51) and a deflector portion (52), said deflector portion (52) being provided on the upper surface of said main body (51), said deflector portion (52) extending from one side of said main body (51) to the other side of said main body (51), the cross-sectional dimension of said deflector portion (52) decreasing in the direction from bottom to top, the side walls of said deflector portion (52) being curved or inclined.

9. A rocket launch platform according to claim 1, characterized in that said rocket launch platform further comprises a locking structure disposed between said launch station (30) and said support platform (20).

10. A rocket launch platform according to claim 1, characterized in that said launch station (30) comprises a gantry (32) and a drive section (33), said rocket body receptacles (31) being arranged on said gantry (32), said drive section (33) comprising a plurality of drive units (331), a plurality of said drive units (331) being arranged at spaced intervals at a lower end of said gantry (32).