A multi-body allosteric satellite platform capable of mimicking
CN119284198BActive Publication Date: 2025-03-07PLA PEOPLES LIBERATION ARMY OF CHINA STRATEGIC SUPPORT FORCE AEROSPACE ENG UNIV
Patent Information
- Application Number
- CN202411833607.8
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Filing Date
- 2024-12-13
- Publication Date
- 2025-03-07
- Estimated Expiration
- 2044-12-13
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Figure CN119284198B_ABST
Abstract
A multi-body conformational satellite platform capable of being shaped, including a platform main body module and a sailboard integrated module; the platform main body module includes four platform main body units and multiple rotation joints, the four platform main body units include a first platform main body unit, a second platform main body unit connected to the bottom side of the first platform main body unit through a rotation joint, a third platform main body unit connected to the top side of the second platform main body unit through a rotation joint, and a fourth platform main body unit connected to the bottom side of the third platform main body unit through a rotation joint; the platform main body unit includes multiple vertically arranged platforms connected by rotation joints; the sailboard integrated module is installed on the platform main body unit in a folded or unfolded cyclic switching state. The present invention can be adjusted to the best launch configuration, which is convenient for carrying and launching into orbit, and can be conformed to a conventional satellite state after entering orbit, and can conceal its own scale characteristics through stacking conformational transformation to avoid collision risks such as space debris.
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Citation Information
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