A connection and separation device for batch launch of satellite groups

A technology for connecting separation devices and satellite groups, applied in the aerospace field, can solve the problems of low utilization of satellite launch space, unfavorable satellite on-orbit deployment and control, unfavorable mass production, etc., to meet the requirements of simplicity and safety, strong equipment adaptability, On-orbit unlocking for safe and convenient effects

Active Publication Date: 2021-07-30
中国星网网络应用有限公司
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  • Application Information

AI Technical Summary

Problems solved by technology

[0003] (1) In the rocket envelope, additional distributors need to be designed for multi-satellite launches, and the utilization rate of satellite launch space is low;
[0004] (2) Each satellite needs to design a separate connection and separation structure and pyrotechnics, the structure is complex, which is not conducive to mass production;
[0005] (3) The separation process is complicated, which is not conducive to the constellation deployment and control of satellites in orbit

Method used

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  • A connection and separation device for batch launch of satellite groups
  • A connection and separation device for batch launch of satellite groups
  • A connection and separation device for batch launch of satellite groups

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Embodiment Construction

[0025] The present invention will be further described below in conjunction with accompanying drawing:

[0026] This embodiment provides a connection and separation device for satellite group batch launch, such as figure 1 As shown, it includes a base 6, a docking mechanism 3, a locking mechanism 8 and an unlocking mechanism; the docking mechanism 3 is connected to the satellite body 1, and a plurality of docking mechanisms 3 are overlapped, and between two adjacent docking mechanisms 3, there is a docking mechanism at the bottom 3 and the base 6 are provided with an elastic mechanism, the two adjacent docking mechanisms 3 contact through the elastic mechanism, and the bottommost docking mechanism 3 (that is, the docking mechanism 3 close to the base 6) contacts the base 6 through the elastic mechanism. catch. Base 6 is connected with docking mechanism 3 by locking mechanism 8, and locking mechanism 8 is used to make docking mechanism 3 be fixed on the base 6, and at this mom...

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Abstract

The invention discloses a connection and separation device for batch launch of a satellite group, which comprises a base, a docking mechanism and a locking mechanism; the docking mechanism is connected to the satellite body, and a plurality of docking mechanisms are overlapped, and the bottommost one is between two adjacent docking mechanisms There is an elastic mechanism between the docking mechanism and the base, the two adjacent docking mechanisms are abutted by the elastic mechanism, and the bottommost one is abutted by the elastic mechanism and the base; the base is connected with the docking mechanism by a locking mechanism, and the locking mechanism is used To fix the docking mechanism on the base. Adopting the scheme provided by the present invention can realize the launch of a large number of satellites at the same time, greatly reduce the launch cost, and provide guarantee for the mass launch of satellites and constellation construction; the design meets the scalability of launching multiple satellites with one arrow and the unity of satellite design and manufacture , the assembly of each satellite before launch is convenient, the requirements are loose, the safety requirements are met during the launch process, and the unlocking in orbit is safe and convenient.

Description

technical field [0001] The invention belongs to the field of aerospace technology, and in particular relates to a connection and separation device for batch launching of satellite groups. Background technique [0002] The connection and unlocking structure between the satellite and the rocket is an important part of the satellite. On the one hand, it provides fixed support for the satellite launch, and on the other hand, it provides the unlocking power when the satellite and the rocket are separated. At present, satellite launches are mainly based on single-satellite launches. In multi-satellite launches, each satellite and the distributor have independent interfaces. The connection and separation methods are simple, widely used, and the technology is mature. With the rapid development of satellites and constellations, the demand for the number of satellites is increasing day by day, especially the rapid development of the global mobile Internet, which makes the demand for t...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64G1/64
CPCB64G1/641B64G1/645B64G1/643
Inventor 杨增俊宋曜廷赵永佳彭维峰李勇周鑫君余弘扬栾欣
Owner 中国星网网络应用有限公司
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