Endurosat 3U Platform for SmallSat Missions - Orbital Transports SmallSat Catalog

3U Cubesat Platform - Endurosat

EnduroSat
Description

Our 3U CubeSat Bus is a fully integrated nanosatellite capable of supporting up-to 1.5U (1.5 kg) payloads. Available with Attitude Determination and Control System (ADCS) with pointing accuracy as high as 0.1 degrees and complete payload integration support, this is our most versatile platform to date.

Included

  • Packed in a protective case
  • Technical information (Datasheet)
  • 10 hours of engineering support
  • Full warranty

Qualification

During the space qualification campaign, EnduroSat CubeSats underwent high level of functional tests to demonstrate the integrity of the 3U CubeSat system. All modules were performing at their nominal level. The tests were performed following the strict specifications of the ESA ECSS-E-ST-10-03C and NASA GEVS: GSFC-STD-7000A standards.

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Additional Information
Available Payload volume:
97 x 97 x 150 mm
Available Mass:
0.5 to 1.5 kg (configuration dependent)
Available Power:
10 to 15 W (orbit and mission dependent)
Power Buses Voltages:
3.3 V, 5 V, Customizable 6-12 V, BCR and battery raw
Data rate in the air:
up to 150 Mbps
Attitude Control:
< 0.1-1 degrees accuracy
Lifetime:
1 – 5 years (orbit dependent)
Documentation

Our 3U CubeSat Bus is a fully integrated nanosatellite capable of supporting up-to 1.5U (1.5 kg) payloads. Available with Attitude Determination and Control System (ADCS) with pointing accuracy as high as 0.1 degrees and complete payload integration support, this is our most versatile platform to date.

Included

  • Packed in a protective case
  • Technical information (Datasheet)
  • 10 hours of engineering support
  • Full warranty

Qualification

During the space qualification campaign, EnduroSat CubeSats underwent high level of functional tests to demonstrate the integrity of the 3U CubeSat system. All modules were performing at their nominal level. The tests were performed following the strict specifications of the ESA ECSS-E-ST-10-03C and NASA GEVS: GSFC-STD-7000A standards.