EnduroSat 1U CubeSat Platform + ADCS + Payload Integration

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

  • Available Payload volume: 97 x 97 x 53 mm3
  • Available Mass: approx. 450 g (waiver process for > 450 g payload)
  • Available Power: 521 mW (orbit and mission dependent)
  • Power Buses Voltages: 3.3/3.7 Battery raw / BCR 5V Max / 5 V
  • Date rate in the air: up to 100 kbps
  • Attitude Control: < 3 degrees accuracy
  • Lifetime: 1 – 5 years (orbit dependent)

Included modules

  • 1x 1U Structure
  • 1x Power Module
  • 1x UHF Transceiver Type II
  • 1x Onboard Computer
  • 1x UHF Antenna
  • 2x Protoboard
  • 1x Solar Panel X/Y
  • 1x Solar Panels X/Y RBF
  • 2x Solar Panels X/Y MTQ
  • 1x Solar Panel Z
  • 1x Solar Panel Z MTQ

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

Package

Custom box

Engineering Support

20 hours

Tech info

Datasheet

Qualification tests

Space qualification tests are performed on all of the Qualification Engineering Model’s subsystems. 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

Technical specifications

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

Images

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