Micro-nano satellite unfolding mechanism

The invention discloses a micro-nano satellite unfolding mechanism which comprises a satellite body, a solar wing assembly, a data transmission antenna assembly, an electric detection antenna assembly, a first rope limiting piece, a first binding rope and a first cut-off mechanism. The solar wing as...

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Bibliographic Details
Main Authors WANG FANRONG, TENG LAI
Format Patent
LanguageChinese
English
Published 03.05.2024
Subjects
AIRCRAFT
ANTENNAS, i.e. RADIO AERIALS
AVIATION
BASIC ELECTRIC ELEMENTS
COSMONAUTICS
ELECTRICITY
PERFORMING OPERATIONS
TRANSPORTING
VEHICLES OR EQUIPMENT THEREFOR
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Summary:The invention discloses a micro-nano satellite unfolding mechanism which comprises a satellite body, a solar wing assembly, a data transmission antenna assembly, an electric detection antenna assembly, a first rope limiting piece, a first binding rope and a first cut-off mechanism. The solar wing assembly comprises a sailboard swinging mechanism, a solar sailboard and a sailboard 180-degree unfolding mechanism; first rope limiting pieces are arranged on the solar panel, the data transmission base bracket and the electric detection connecting rod; the first binding rope is wound on the outer side of the satellite body through the first rope limiting piece and enables the solar wing assembly, the data transmission antenna assembly and the electric detection antenna assembly to be kept in a folded state. The first cut-off mechanism is arranged on the satellite body, and the first cut-off mechanism and the first binding rope are arranged correspondingly. The solar wing, the data transmission antenna and the elect
Bibliography:Application Number: CN202410319995