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Braking sail derailment device for cube satellite

A cube satellite and braking sail technology, applied in the field of spacecraft de-orbit, can solve the problems of de-orbit and no space to install a braking sail device, and achieve the effects of ensuring reliability, reducing the difficulty of ground control, and reducing manufacturing costs

Pending Publication Date: 2018-01-05
NANJING UNIV OF SCI & TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0010] The object of the present invention is to provide a deorbiting device for cubesat braking sails, which is suitable for deorbiting of three cubesats of 1U, 2U and 3U, and can not only solve the problem that the cubesat cannot be deorbited within a specified time after completing the task The problem of space debris, but also solves the problem that there is no space to install the brake sail device in the smaller cube star

Method used

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  • Braking sail derailment device for cube satellite
  • Braking sail derailment device for cube satellite
  • Braking sail derailment device for cube satellite

Examples

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Embodiment

[0041] Embodiment: Taking a double-unit cube star as an example

[0042] combine figure 1 , figure 2 , image 3 , Figure 4 , a CubeSat braking sail deorbiting device, its main part occupies a space of φ70mm×60mm, and it is fixedly connected to the bottom of the dual-unit CubeSat through the top mounting panel 3, so as not to occupy the space in the CubeSat.

[0043] The cube satellite braking sail deorbiting device includes a locking device 1 , a storage mechanism 2 , an installation panel 3 , a conical spring 4 , an unfolding mechanism 5 and a membrane sail 6 . The locking device 1 is fixed on the top surface of the installation panel 3, the storage mechanism 2 is fixed on the bottom surface of the installation panel 3, the conical spring 4, the unfolding mechanism 5 and the film sail 6 are all arranged in the storage mechanism 2, and the conical spring 4 has a large diameter One end of one end is fixedly connected with installation panel 3, and one end with small diame...

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Abstract

The invention discloses a braking sail derailment device for a cube satellite. The braking sail derailment device comprises a locking device, a storage mechanism, a mounting panel, a conical spring, an unfolding mechanism and a diaphragm sail. The locking device is fixed on the top face of the mounting panel. The storage mechanism is fixed on the bottom face of the mounting panel. The conical spring, the unfolding mechanism and the diaphragm sail are arranged in the storage mechanism. The large-diameter end of the conical spring is fixedly connected with the mounting panel, and the small-diameter end of the conical spring is fixedly connected with the unfolding mechanism. The diaphragm sail is tied to the unfolding mechanism. The braking sail derailment device is fixedly connected to the bottom of the satellite through the mounting panel at the top, so that the space inside the satellite is not occupied. After receiving a command from the ground, the locking device releases a central shaft in the unfolding mechanism, and a strap elastic mast wound on the central shaft drives the diaphragm sail fixed on the mast to be unfolded by releasing elastic potential stored in the mast. According to the invention, the diaphragm sail is unfolded to increase the cross-sectional area in the flight direction of the cube satellite, and the atmospheric resistance of the cube satellite is increased, so that the cube satellite derails quickly.

Description

technical field [0001] The invention belongs to the field of spacecraft de-orbiting, and in particular relates to a cube satellite braking sail de-orbiting device. Background technique [0002] Space debris mainly includes man-made objects in near-Earth space other than active spacecraft. The space where they are produced and operated is generally in the area where most spacecraft currently fly. The main sources include rocket bodies, failed spacecraft, and mission-related objects. Fragments and Fragments. In recent years, with the continuous development of aerospace technology, the number of space debris in the earth's orbit has also been increasing, which seriously threatens the safety of effective spacecraft in orbit and also lays hidden dangers for the development of human space technology in the future. How to slow down the growth of space debris has become an urgent problem at home and abroad. The Inter-Agency Space Debris Coordination Committee (IADC) recommends tha...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G1/62
Inventor 梁振华韩戴如张翔钱鹏俊
Owner NANJING UNIV OF SCI & TECH
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