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Micro/nano-satellite multi-star adaption portion deploy device and application

A micro-nano satellite and deployment device technology, applied in the field of micro-nano satellite, can solve the problems of micro-nano satellite deployer single function, device customization, high development cost, unfavorable modularization, large-scale production, etc., to meet the requirements of orbital deployment requirements, low-cost multi-satellite adaptation, and the effect of low-cost design

Active Publication Date: 2015-08-05
THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD
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Problems solved by technology

[0005] However, the existing micro-nano-satellite deployers have single functions and low adaptability, and can only realize functions for one type of micro-nano-satellite. At the same time, their devices are customized and their development costs are high, and they do not use modularization and large-scale production, which is also not conducive to Lower cost of launch

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  • Micro/nano-satellite multi-star adaption portion deploy device and application
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  • Micro/nano-satellite multi-star adaption portion deploy device and application

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Embodiment Construction

[0028] In order to make the object, technical solution and advantages of the present invention clearer, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention. In addition, the technical features involved in the various embodiments of the present invention described below can be combined with each other as long as they do not constitute a conflict with each other.

[0029] The device in the present invention includes a deployer and a platform interface, the platform interface is provided with a computer, and the platform interface connects the deployer to the satellite platform, so that the deployer and the satellite platform are physically and electrically connected; the deployer is used to simultaneously accommodate Multiple micro-nano-satellites of diffe...

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Abstract

The invention discloses a micro / nano-satellite multi-star adaption portion deploy device which comprises a deploy instrument and a platform interface. The platform interface is used for achieving physical and electric connection between the deploy instrument and the satellite platform. The deploy instrument comprises a support assembly and an ejection assembly. The support assembly comprises partition plates (1) and lateral plates (2). A slot (11) is formed in each partition plate (1), and the lateral plates (2) are clamped in the slots (11). The plurality of partition plates arranged in parallel and the plurality of lateral plates of different specifications are utilized to form a plurality of layers of cases with different sizes to contain micro / nano satellites of different specifications. The ejection assembly (3) is used for ejecting the micro / nano satellites. The deploying instrument can contain the micro / nano satellites of various specifications and launch the satellites, and is good in generality and low in cost.

Description

technical field [0001] The invention belongs to the field of micro-nano-satellites, and more specifically relates to a micro-nano-satellite multi-satellite adaptive deployment device capable of realizing multi-satellite deployment function and its application. Background technique [0002] The increase in volume and quality of spacecraft and the complexity of functions have led to rapid increases in research, development, production, launch, operation and maintenance costs of spacecraft, while technical reliability and management safety have declined, causing failure rate increases. The small spacecraft has become a research hotspot due to its strong adaptability, mobility, and combinable applications. Micro-nano-satellites are typical representatives of small spacecraft. In recent years, various application technologies based on micro-nano-satellite platforms have developed vigorously, and the demand for launching micro-nano-satellites has gradually increased. [0003] Mi...

Claims

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Application Information

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IPC IPC(8): B64G1/64
Inventor 王星又项斌胡长伟张斌梁纪秋
Owner THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD
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