Integrated launching pad

A launch pad and integrated technology, applied in the direction of rocket launchers, offensive equipment, weapon types, etc., can solve the problems of high construction costs, large-scale products, large-scale land occupation, etc., and achieve small footprint and time-saving deployment The effect of short, reduced scale and occupied area

Active Publication Date: 2018-04-20
CHINA ACAD OF LAUNCH VEHICLE TECH
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  • Abstract
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  • Claims
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AI Technical Summary

Problems solved by technology

[0004] The technical problem of the present invention is to overcome the deficiencies of the prior art and provide an integrated launching platform to solve the problem that the current reusable aircraft launching platform occupies too much land, the construction cost is too high, the product scale is large, and it cannot be quickly launched. The problem with mobile launches

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  • Integrated launching pad

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Embodiment Construction

[0025] In order to make the purpose, technical solution and advantages of the present invention clearer, the following will further describe the public implementation manners of the present invention in detail with reference to the accompanying drawings.

[0026] The invention discloses an integrated launching platform, which has the advantages of compact structure, small floor space, simple and reliable, fast and maneuverable, ready to withdraw at any time, short preparation time, reusable for many times, etc. Require. The integrated launch pad described in the present invention can be applied in suborbital reusable vehicle projects, and meanwhile, can be extended to other similar aircraft or rocket projects.

[0027] refer to figure 1 , shows a schematic structural view of an integrated launching platform in an embodiment of the present invention. In this embodiment, the integrated launching platform includes: a base 1 , a launching platform 2 , a deflector 4 and a swing r...

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Abstract

The invention discloses an integrated launching pad which comprises a base, a launching pad body, a deflector and a swing rod. The launching pad body, the deflector and the swing rod are fixed to thebase. An aircraft is mounted on the launching pad body, and the deflector is located below the launching pad body. The launching pad body, the aircraft and the deflector are located on the same axis.The swing rod can swing along the fixed supporting point by a first set angle. When the aircraft is fixed, the end, away from the ground, of the swing rod is in contact with the aircraft and is used for supporting and fixing the aircraft. By means of the integrated launching pad, the problems that at present, a reusable aircraft launching pad is too large in occupied scale, too high in construction cost and huge in product scale, and mobile launching cannot be achieved fast are solved.

Description

technical field [0001] The invention belongs to the technical field of suborbital reusable vehicles, and in particular relates to an integrated launching platform. Background technique [0002] Suborbital reusable vehicles have the characteristics of short launch time, repeated use, and multiple launches. The launch pad should be able to meet the characteristics of short preparation time, compact and reliable structure, small footprint, good economy, and repeated use. However, the launch pads used by domestic and foreign models are relatively large in scale, occupy a large area, and have poor adaptability. [0003] For example, the United States and other countries mostly adopt the vertical transfer method, and the launch pad needs to ensure the reliable fixation of the rocket or aircraft during the transfer process, and the scale is large. For another example, Russia and other countries adopt the method of horizontal transfer and vertical launch, but the launch and support...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F41F3/04
CPCF41F3/04
Inventor 赵建波杜朋飞袁园赵胜
Owner CHINA ACAD OF LAUNCH VEHICLE TECH
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