EnduroSat 1U CubeSat Platform + ADCS + Payload Integration

Up to 50%
payload volume
Up to 5X faster
production and delivery
Up to 5x better
Designed as a
multipurpose platform
Capability for
mass production
Ideal test bed for new technologies
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EnduroSat 1U CubeSat Platform + ADCS + Payload Integration

  • Available Payload volume: 97 x 97 x 53 mm3
  • Available Mass: 453 g (waiver process for > 453 g payload)
  • Available Power: 521 mW (orbit and mission dependent)
  • Power Buses Voltages: 3.3/3.7 Battery raw / BCR 5V Max / 5 V
  • Payload Data Downlink: 41 MB per pass S-Band
  • Telemetry and Telecommand: 2000 / 12000 baud rate UHF
  • Attitude Control: < 3 degrees accuracy
  • Lifetime: 1 – 3 years (orbit dependent)

Included modules

  • 1x Power Module
  • 1x S-Band/UHF Communication Module
  • 1x Onboard Computer
  • 1x S-Band Patch Antenna
  • 1x UHF Antenna
  • 1x Structure 1U
  • 2x Solar Panels X/Y
  • 2x Solar Panels X/Y MTQ
  • 1x Solar Panel Z MTQ
  • 2x Protoboard

Additional features

  • Payload Integration after compatibility verification;
  • Functional verification with integrated payload;
  • Attitude Determination and Control Software;
  • Dedicated X/Y Panel with Remove before flight pin and system check interface
  • RTOS
  • Software drivers;
  • Cables;
  • 20 of hours engineering support

Included with 1U CubeSat + ADCS + Payload


Custom box

Engineering Support

20 hours

Tech and User information

USB Drive

Qualification tests

Space qualification tests are performed on the Qualification Engineering Model. Qualification tests level and duration follow the ESA standard ECSS-E-ST-10-03C and GEVS: GSFC-STD-7000A.

Functional Test
Random Vibration
Sinusoidal Vibration
Pyroshock Test

Thermal Cycling
Thermal Vacuum
Total Ionizing Dose – planned in the coming weeks

Technical specifications

Please, contact us for the complete technical specifications of 1U CubeSat Platform + ADCS + Payload Integration.


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