Subsystem Summary: The Attitude Determination and Control subsystem (ADCS) is the navigational core of AcubeSAT.

Subsystem Summary: The Communications (COMMS) subsystem is responsible to reliably transfer the largest possible volume of scientific and diagnostic data between the satellite and the Earth, by developing the necessary On-Board and Ground Station hardware and software.

Subsystem Summary: The Communications (COMMS) subsystem is responsible to reliably transfer the largest possible volume of scientific and diagnostic data between the satellite and the Earth, by developing the necessary On-Board and Ground Station hardware and software.

Subsystem Summary: The Communications (COMMS) subsystem is responsible to reliably transfer the largest possible volume of scientific and diagnostic data between the satellite and the Earth, by developing the necessary On-Board and Ground Station hardware and software.

Position Overview: The Marketing team works in the shadows to support the team creatively, socially, and financially.

Position Overview: The Marketing team works in the shadows to support the team creatively, socially, and financially.

Position Overview: The Marketing team works in the shadows to support the team creatively, socially, and financially.

Subsystem Summary: On-Board Software is responsible for designing, implementing and maintaining software for the embedded systems of the satellite.

Subsystem Summary: The On-Board Computer or On-Board Data Handling subsystem is responsible for designing and implementing the hardware and software for microcontrollers that control all basic functions of the satellite.

Subsystem Summary: The On-Board Computer or On-Board Data Handling subsystem is responsible for designing and implementing the hardware and software for microcontrollers that control all basic functions of the satellite.

Subsystem Summary: Spacecraft Operations is responsible for maintaining the ground mission control software, implementing the Telecommand and Telemetry services, automating nominal pass procedures and operating as the “command center” for on-board processes.

Subsystem Summary: Spacecraft Operations is responsible for maintaining the ground mission control software, implementing Telecommand and Telemetry services, automating pass procedures and operating as the “command center” of on-board processes.

Subsystem Summary: The structural subsystem is responsible for the design of the physical layout of the satellite and the verification of its structural integrity.

Position Overview: The Science Unit is responsible for designing and implementing the mission experiment, probing the dynamic response of S.

Position Overview: The Science Unit’s success is deeply rooted in its capacity to not only design theoretical experiments but also to prototype, test, and perfect its systems in real-world conditions.

Position Overview: The Science Unit is responsible for designing and implementing the mission experiment, studying how the radiation and microgravity conditions prevalent in the Low Earth Orbit affect yeast cells at a molecular level.

Position Overview: The Science Unit is responsible for designing and implementing the mission experiment, studying how the radiation and microgravity conditions prevalent in the Low Earth Orbit affect yeast cells at a molecular level.

Overview: The Systems Engineering subteam is tasked with ensuring the correct and reliable functionality of the spacecraft and the system level design coordination of all subsystems, while also ensuring compliance with a wide array of standards.

Subsystem Summary: The Thermal subsystem is responsible for ensuring that the satellite’s components shall not exceed their operating and non-operating temperatures.