My mind about CubeSat

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CubeSat launch entails decision-making regarding three primary issues: communication, energy supply, and maneuverability. Communication involves one-way transmission from the satellite, two-way communication with double-sided information exchange or broadcasting to users worldwide. Energy provision is crucial for powering all satellite systems, including communication, and can be sourced through solar panels or isotope sources based on alpha or beta decay. Maneuverability involves changes in orbit or spatial orientation, depending on the power plant and onboard energy source. For CubeSat manufacturing, a framework concept proposes a three-part structure consisting of closed contour and two covers with locks. This design eliminates fasteners and allows for 3D printing of all main components. The panel can have any perforation, edges, or slots as required. BIMETALLIC plates, or thermal relays, can be used for automatic opening in the cold of space. Piezo crystals can also open covers with minimal energy input, controlled by operators. This framework offers solutions for urgent orbit changes against space debris and sudden orbit adjustments to dodge aliens, although maneuverability may not always be necessary. The provided CAD model represents a conceptual design only and should not be considered an actual structure. Despite the challenges presented by English, it is hoped that the message has been clearly conveyed.