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Modular spacecraft capable of being deformed in orbit

A space vehicle and modular technology, which is applied to aerospace vehicles, aircraft, and aerospace vehicle power supply systems, etc., can solve the problems of failing to achieve on-orbit assembly and splicing of modular satellites, failing on-orbit tests, etc. Achieve long service life, low cost and fast on-orbit response

Pending Publication Date: 2018-07-27
TSINGHUA UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Existing programs at home and abroad, such as "Phoenix Project", "F6", "iBOSS" program, "Space Robot" program, etc., basically all adopt heterogeneous design, and none of them have passed the in-orbit test and failed to achieve isomorphism On-orbit assembly and splicing of modular satellites, as well as the completion of specific tasks

Method used

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  • Modular spacecraft capable of being deformed in orbit
  • Modular spacecraft capable of being deformed in orbit
  • Modular spacecraft capable of being deformed in orbit

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Embodiment Construction

[0032] Embodiments of the present invention are described in detail below, examples of which are shown in the drawings, wherein the same or similar reference numerals designate the same or similar elements or elements having the same or similar functions throughout. The embodiments described below by referring to the figures are exemplary only for explaining the present invention and should not be construed as limiting the present invention.

[0033] In describing the present invention, it should be understood that the terms "center", "longitudinal", "transverse", "length", "width", "thickness", "upper", "lower", "front", " Back", "Left", "Right", "Vertical", "Horizontal", "Top", "Bottom", "Inner", "Outer", "Clockwise", "Counterclockwise", "Axial", The orientation or positional relationship indicated by "radial", "circumferential", etc. is based on the orientation or positional relationship shown in the drawings, and is only for the convenience of describing the present invent...

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PUM

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Abstract

The invention discloses a modular spacecraft capable of being deformed in orbit. The modular spacecraft comprises basic module cell bodies, and each of the basic module cell bodies comprises a frame and a functional module. The frame is provided with magnetic connecting pieces, and two of the basic module cell bodies can be connected by connecting the magnetic. The functional module is mounted onthe frame, and the functional module is used for performing a predetermined task of the basic module cell bodies. According to the modular spacecraft capable of being deformed in orbit, since the functional module on the basic module cell bodies enables the basic module cell bodies to perform the predetermined task, and the magnetic connecting pieces on the frame can connect a plurality of basic module cell bodies, the modular spacecraft has the advantages of flexible structure, low cost, fast response speed in orbit and long service life, and the problems of complex design, high cost and difficulty in replacing parts in the past are solved.

Description

technical field [0001] The patent of the present invention relates to the overall design technology of space vehicles, and specifically relates to a modular space vehicle that can change configurations in orbit. Background technique [0002] With the rapid development of aerospace technology, information technology, new materials and advanced manufacturing technology, the use of outer space will undergo revolutionary changes, and the miniaturization and low-cost launch of space systems will become an important trend in future aerospace development. In the future "elastic dispersion" type space system, various space vehicles will be able to complete. From the perspective of technological development trends, it will have the characteristics of modularization, intelligence, reconfigurability, maintainability, and recombination. [0003] For the design and connection technology of reconfigurable multi-agents, there is no perfect solution yet. Existing programs at home and abro...

Claims

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Application Information

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IPC IPC(8): B64G1/10B64G1/44
CPCB64G1/10B64G1/443
Inventor 刘孙相与张鑫焱赵孔亚詹亚锋李贵涛
Owner TSINGHUA UNIV
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