From initial conceptual design to flight-ready hardware, we specialize in high-performance satellite platforms and critical structural components. We utilize advanced additive manufacturing and precision assembly to ensure maximum durability and efficiency in the harsh space environment.
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Core Spacecraft Engineering Subsystems [1]
A spacecraft must operate reliably in a vacuum while enduring extreme radiation and dramatic thermal cycling. To survive, it relies on several interdependent subsystems:
Structures and Mechanisms: The physical chassis, typically optimized for minimum mass and maximum stiffness to withstand immense launch vibrations.
Attitude Determination and Control (ADCS): Tracks spatial orientation and uses sensors (star trackers) and actuators (reaction wheels) to keep payloads or solar panels pointed correctly.
Command and Data Handling (C&DH): The “brain” of the vehicle, running flight software and processing commands.
Telemetry, Tracking, and Command (TT&C): The communications link that routes sensor data back to Earth and receives mission commands.
Electrical Power Subsystem (EPS): Generates power via solar arrays and stores energy in batteries managed to withstand continuous orbital cycling.
Thermal Control Subsystem (TCS): Regulates temperatures using insulation, radiators, heat pipes, and louvers to protect internal components from absolute cold and direct solar heat.
