The 1U Standard Platform enables simple experiments in space for signal reception and Earth Observation. It is a good choice for projects that require a small platform for doing nanosatellite integration and in-space operation training.
The satellite platform has been used in several Academic programs since 2014.
 

Main Application Areas1U Exterior

  • Radio communication
  • Earth Observation Experiments
  • Academic programs


Highlights

The 1U standard platform is tested and ready for integration of your payload, or it can be upgraded with a GomSpace provided payload consisting of a RGB camera with a 35 mm lens providing 60m per pixel resolution at 650km orbital altitude. 


Integration and Environmental Tests

The platform and its elements have been qualified according to the GomSpace qualification program, which includes tests in: Vibration, thermal cycling, heated vacuum, radiation and thermal stress.

The platform is tested and ready for payload integration. Payload integration is offered by GomSpace as a paid service. 

 

Technical information
 

Platform

Size

1U

Peak Power

3.4W

Platform power consumption

 

Battery capacity

20W

Platform mass

0.95 kg

Platform lifetime

< 1 year

 

Payload1

Payload space

0.3U

Average payload power

Depending on orbit - contact our sales department for info

Max. payload mass1

1 kg

Payload Interfaces

CAN bus

Power Bus

3.3V, 5V

1Max. available payload mass depends on deployer
 

Subsystems

Flight Heritage since

Power System

Power system with 2 onboard Batteries, Solar Panels on all satellite faces.

2014

Mechanics

1U CubeSat Structure and full Harness Set

2014

Command & Management

Preinstalled software package for Satellite Control, Mission Library for Flight planning and data collection,

2014

Communication system

Communication system with On-Board Computer, UHF radio and antenna and Flight Preparation Panel for testing.

2014

ADCS System

ADCS software for basic stabilization and preinstalled example code configured for system diagnostics. Basic Attitude Determination and Control System with integrated magnetorquers in the solar panels for basic stabilization and alignment of satellite

2014

 

Documentation

  • Product manuals and datasheets

  • Platform qualification program description

  • Platform checkout certificate

  • Integration manual and test plan


Communication interfaces for Payloads

  • CAN bus


Available services and options

  • Integration of customer payload

  • Engineering support

  • LEOP support

  • Ground station elements or operations

 

Lead time

For a standard platform delivery without payload integration, lead time is 4-6 months from receipt of order. 

 

For further information about the 1U Standard Platform contact our sales department

contact us
 
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