A space debris-specific orbital removal device and method of using the same
A space debris and removal device technology, applied in the aerospace field, can solve problems such as low recovery efficiency, complex structure, and high cost, and achieve the effects of thorough removal, reduced difficulty, and low cost
Active Publication Date: 2018-12-25
NORTHWESTERN POLYTECHNICAL UNIV
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- Application Information
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Problems solved by technology
[0005] The purpose of the present invention is to provide a space debris specific orbit removal device to solve the problems of complex structure, high cost and low recovery efficiency of space debris collection devices in the prior art
Method used
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[0029] The present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments.
[0030] The invention provides a space debris specific orbit removal device, such as figure 1 As shown, it includes a bowl-shaped structure for collecting and storing space debris, and the outer bottom of the bowl-shaped structure is connected to the fixed frame through a connecting part.
[0031] Such as figure 2 As shown, the connecting part is used to control the expansion of the bowl-shaped structure along its connection end and fit on the outer wall of the fixed frame when the mission spacecraft carries the space debris specific orbit removal device, and when the space debris specific orbit removal device is out of the mission When the spacecraft, it breaks away from the outer wall of the fixed frame and forms a bowl-shaped structure; in this way, when the mission spacecraft transports the device, space can be saved so that more pieces ...
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The application discloses vacant debris designated orbit clearing installation, including a bowl shape construction for receiving and depositing vacant debris, the outside bottom of the bowl shape construction joins with a fixed skeleton through a connection department; the connection department controls bowl shape construction and unfolds at a connection end of the bowl shape construction and adheres on fixed skeleton outside wall, when playing a role of designated orbit clearing installation for task aviation equipment carrying vacant debris, the control bowl shape construction detaches fixed skeleton outside wall and takes bowl shape, at the time when vacant debris designated orbit clearing installation detaches from task aviation equipment; the fixed skeleton remote department by bowl shape construction fixes a head engine, the middle of head engine and bowl shape construction, along the head engine to bowl shape construction direction in sequence steadily assembles a central plate, pose inspecting and testing installation and power supply; bowl shape construction steadily assembles more tables of little mould engine, every little mould engine joins to central plate by getting across conduit wire; head engine suits for adjusting engaged installation within vacant motion orbit; engaged installation constructs plainly, costs less, recovers at high performance rate.
Description
【Technical field】 [0001] The invention belongs to the field of aerospace technology, and in particular relates to a device for clearing specific orbits of space debris and a method for using the same. 【Background technique】 [0002] Space debris refers specifically to the waste and its derivatives produced by human beings in space activities. There are many sources of space debris. No one can count the exact number of space debris. At present, human beings can only track and monitor debris with a diameter of more than 10 centimeters. It is estimated that there are tens of millions or even hundreds of millions of debris smaller than 1 centimeter. It is impossible to avoid colliding with it at all, and we can only deal with it by strengthening our own protection capabilities. [0003] Space debris, especially small space debris (less than 1 cm), is difficult to monitor and track effectively due to their large number and wide distribution. The pollution they cause to the space...
Claims
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IPC IPC(8): B64G4/00B64G1/66
CPCB64G1/66B64G4/00
Inventor 赵志新魏祥庚张晓亮李昊远周楠怡何厚辛
Owner NORTHWESTERN POLYTECHNICAL UNIV