Chemical molecule satellite with strong deformability

Abstract

The invention discloses a chemical molecule satellite with high deformability. The chemical molecule satellite comprises an atomic satellite and a single mechanical arm and / or double mechanical arms. The atomic satellite is constructed to be in a truncated octahedron shape, the atomic satellite comprises eight first functional areas and six second functional areas, and at least one of the first functional areas and the second functional areas is provided with a connecting structure; the single mechanical arm comprises a rod-shaped arm body, a first connecting part and a second connecting part, the first connecting part and the second connecting part are arranged at the two ends of the arm body, the first connecting part and the second connecting part can at least partially rotate and bend relative to the arm body, and both the first connecting part and the second connecting part can be connected to a connecting structure. The double mechanical arms are formed by connecting two adjacent single mechanical arms. The chemical molecule satellite can be flexibly deformed to form various different configurations, can perform quick response, has higher survival adaptability, and can meet various different task requirements.

Description

technical field [0001] The invention relates to the technical field of satellite structures, in particular to a chemical molecular satellite with strong deformability. Background technique [0002] Artificial satellites are spacecraft that follow the laws of orbital mechanics to fly around the earth or other planets for a long time and perform on-orbit missions. Artificial satellites can achieve a variety of functions, such as ground monitoring, astronomical observation, communication relay and scientific research. Existing artificial satellites include traditional satellites and micro-nano satellites. Compared with traditional satellites, micro-nano satellites have small size, low power consumption, short development cycle, and can be formed into a network, which can complete many complex space tasks at a lower cost. However, due to the small size of micro-nano satellites and the limited size of the payload platform, there is limited space to receive on-orbit upgrades to ...

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Problems solved by technology

However, the structure of the cell-star assembly is relatively simple, and the functions that can be realized are limited. It is still difficult to adapt to complex and diverse tasks. Orbits are assembled to form a specific shape, and the combined form of cells and stars limits its ability to reconfigure and cannot achieve rapid deformation

At the same time, there are delays and leaks in the communication between the various satellite modules in the distributed configuration. The ability of the satellite module to perform space missions

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