Satellite and launch vehicle connection and separation mechanism

A technology for connecting and separating mechanism and star arrow, applied in the field of star-arrow connecting and separating mechanism, can solve the problems of insufficient pressing force, uncontrollable pressing force, unreasonable spring structure, etc. Simple and compact structure

Inactive Publication Date: 2016-11-09
SHANGHAI AEROSPACE SYST ENG INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The existing connection and separation mechanisms generally use pyrotechnic connection to unlock, which has the following disadvantages: large impact; generally only has one installation surface, and the installation layout is inconvenient; the structure is relatively complicated and the cost is high
There are also some box-type separation mechanisms, the spring structure is unreasona

Method used

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  • Satellite and launch vehicle connection and separation mechanism
  • Satellite and launch vehicle connection and separation mechanism
  • Satellite and launch vehicle connection and separation mechanism

Examples

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Example Embodiment

[0025] In order to make the above objects, features and advantages of the present invention more comprehensible, specific implementations of the present invention will be described in detail below in conjunction with the accompanying drawings.

[0026] In the following description, numerous specific details are set forth in order to provide a thorough understanding of the present invention. However, the present invention can be implemented in many other ways different from those described here, and those skilled in the art can make similar extensions without violating the connotation of the present invention, so the present invention is not limited by the specific implementations disclosed below.

[0027] see figure 1 and 2 , The star-arrow connection and separation mechanism of this embodiment includes: guide rail 1, rear end cover 4, front frame 2, separation spring 6, push plate 11, hatch and connection unlocker 5. It is used to realize the connection and separation betwe...

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PUM

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Abstract

The invention provides a satellite and launch vehicle connection and separation mechanism, comprising a guide rail, a rear end cover, a front end frame, a separation spring, a push plate, a cabin door and a connection unlocking device, wherein the rear end cover is connected to the rear end of the guide rail; the separation spring is arranged in the guide rail and can stretch and retract along the direction of the rail; the push plate is arranged at the front end of the separation spring and is driven by the separation spring to move frontward or backward; the front end frame is connected to the front end of the guide rail; the cabin door is hinged to one side edge of the front end frame; when the front end frame is covered, a satellite is tightly pressed on the push plate and the separation spring, so that satellite and launch vehicle connection is realized; when the front end frame is opened, the separation spring and the push plate are released to frontward push out the satellite, so that satellite and launch vehicle separation is realized; the connection unlocking device is used for locking or unlocking the cabin door in a non-pyrotechnic door. The satellite and launch vehicle connection and separation mechanism has the advantages of low impact, simple structure, light weight, high separation precision, convenience in installation, low cost, high reliability and the like.

Description

technical field [0001] The invention relates to the connection and separation fields such as star-arrow separation and inter-stage separation, and in particular to a star-arrow connection and separation mechanism. Background technique [0002] At present, the rapid development of CubeSat (CUBESAT) requires a connection and separation mechanism adapted to the launch of the CubeSat, which is used to realize the connection and separation of the satellite and rocket during the delivery of the CubeSat. The existing connection and separation mechanisms generally use pyrotechnic connection to unlock, which has the following disadvantages: large impact; generally only has one installation surface, and the installation layout is inconvenient; the structure is relatively complicated and the cost is high. There are also some box-type separation mechanisms with unreasonable spring structures or unreasonable push plate structures, which lead to poor separation accuracy, and even have pro...

Claims

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Application Information

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IPC IPC(8): B64G1/64
CPCB64G1/641
Inventor 王金童王勇龚星如汪全
Owner SHANGHAI AEROSPACE SYST ENG INST
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