Saltar al contenido principal
Technology

The CubeSat

Discover the technology behind our space mission: a nanosatellite with 10 integrated subsystems working in perfect harmony.

General Specifications

Type
CubeSat 1U
Dimensions
10 x 10 x 10 cm
Mass
< 1.33 kg
Orbit
LEO (~400 km)
Lifespan
1-2 years
Power
2W average

Subsystems

Each component is essential for mission success

Payload

Earth surface image capture system using high-resolution camera and specialized sensors.

  • 5MP resolution camera
  • Multispectral sensors
  • 16GB storage

On-Board Computer (OBC)

The brain of the satellite, responsible for processing data, executing commands, and coordinating all subsystems.

  • ARM Cortex-M4 processor
  • Real-time operating system
  • Hardware redundancy

Communications (COMMS)

Bidirectional link system between the satellite and ground station for data transmission and telecommands.

  • UHF/VHF band
  • AX.25 protocol
  • Deployable antenna

Thermal Control (TCS)

Keeps all components within their operational temperature range using passive and active techniques.

  • Passive radiators
  • MLI (multilayer insulation)
  • Temperature sensors

Attitude Determination and Control (ADCS)

System that determines and controls the satellite's orientation in space to correctly point instruments.

  • Magnetometers
  • Gyroscopes
  • Reaction wheels

Ground Station (GS)

Ground control and monitoring center that receives telemetry and sends commands to the satellite.

  • High-gain Yagi antenna
  • Tracking software
  • Operations center

Mechanical Structure

Chassis that protects all internal components and complies with CubeSat standards for deployment.

  • Aluminum 6061-T6
  • CubeSat 1U standard
  • Deployment rails

Space Manufacturing

Manufacturing and assembly processes following aerospace quality standards.

  • Class 100,000 clean room
  • Vibration testing
  • Quality inspection

Power (EPS)

Electrical power generation, storage, and distribution system for all subsystems.

  • Triple-junction solar panels
  • Li-ion batteries
  • Voltage regulators

Propulsion

Orbital maneuvering system for altitude adjustments and deorbiting at end of mission.

  • Electric propulsion
  • Attitude control
  • Passive deorbiting