Linking Earth to the Extraordinary

Your Rover's Cosmic Connector

How CanSat works

CanSat is an international project, which allows students to test their strength in various fields, such as physics, engineering and networking. It is based on a primary mission, which is compulsory, and a secondary mission, which the competitors have to come up with.

Esero

esa-logo esero-logo
small satelink logo all white

Research with us

Find out more about our project by taking a look at the model of our CanSat or exploring our recent Critical Design Review report.

Missions

Primary mission:

As the regulations require, our CanSat will monitor its altitude while falling using a BMP 280 temperature and pressure sensor; connected to the Adafruit Feather M0, the sensor will activate and using the pressure – temperature correlation formula:

At 1Hz, will transmit the readings once per second through a 433Mhz LoRa RFM96 radio module with an omnidirectional antenna. The data will then be graphed out to provide us with the descent rate. Knowing the crosswind value and the rate of change of altitude, we will be able to better estimate the position of the can as it falls on the ground.

Secondary mission:

Our CanSat establishes a two-way communication link with the ground station, using Lora RFM96 modules on both ends. It receives information from the ground station when not transmitting primary mission data, saving it on a micro-SD card. Commands are then relayed to a rover equipped with a directional receiver antenna, allowing task execution. This approach overcomes the limitation of direct control from Earth due to a significant distance of over 3 km. The secondary mission is a technological demonstration, resembling an ExoMars mission, optimizing communication through a relay satellite. This allows the rover to carry a more compact, lighter antenna, enhancing speed, reducing weight, and enabling the incorporation of additional sensors for more comprehensive data collection. Mission success hinges on the CanSat effectively transmitting and executing commands through the rover.

Our CanSat body was designed in Autodesk Fusion 360 for a precise 3D model. Using a Prusa 3D printer, we'll construct structural layers with Polylactic Acid or ColorFabb XT filament, reinforced with 20% carbon fiber for enhanced precision and rigidity. The CanSat comprises four main architectural components.

  • External Casing: Protects internal components during flight and absorbs impact during landing. Cylindrical, 112mm in height, 66mm external diameter, with 15% infill for added strength.
  • Internal Casing: Houses all avionics and components, securely mounting the motherboard with screws. Three AA batteries are distributed between the casing base and the main chamber. Cylinder-shaped, with an external diameter of 60.5mm, internal diameter of 49mm, and optimized for mass with holes. Features a 30% infill for component safety.

Ground Station (PC):
The main ground station is pivotal for both primary and secondary missions. The BMP280 sensor records temperature and pressure on the CanSat, and the data is transmitted to the ground station via the LoRa RFM96 Ra-02 radio module. Communication involves a 3-4 element cross yagi antenna with directional 10dB gain for extended reach. The ground station manages two-way communication, displaying altitude using data software and storing it on the on-ground PC. Additionally, it dispatches stored commands to the CanSat for the secondary mission.

Rover Station:

The Rover, powered by a 3000mAh battery, follows Arduino commands, supported by spring suspension for component weight. Arduino Nano ESP32 acts as the onboard computer, receiving and saving Can data and commands. It controls vehicle movement. The Yagi antenna ensures communication with a 3-4 element or cross yagi design, receiving data without transmitting back to the can.

The CanSat body

Our CanSat body was designed in Autodesk Fusion 360 for a precise 3D model. Using a Prusa 3D printer, we'll construct structural layers with Polylactic Acid or ColorFabb XT filament, reinforced with 20% carbon fiber for enhanced precision and rigidity. The CanSat comprises four main architectural components.

External casing:

Protects internal components during flight and absorbs impact during landing. Cylindrical, 112mm in height, 66mm external diameter, with 15% infill for added strength.

Internal casing:

Houses all avionics and components, securely mounting the motherboard with screws. Three AA batteries are distributed between the casing base and the main chamber. Cylinder-shaped, with an external diameter of 60.5mm, internal diameter of 49mm, and optimized for mass with holes. Features a 30% infill for component safety.

Our Team

Our Partners

Our Sponsors

Contact Us

by email if you want to become a sponsor, help us with the project or simply learn more about it