LEOS-100 [small satellite systems]

LEOS-100 takes small satellites above and beyond. It builds on the proven LEOS-50 avionics but pulls all the stops on performance. There are two versions of LEOS-100: LEOS-100HR with body mounted panels supports large high precision instruments with 50cm GSD earth observation and LEOS-100HP supports support Missions up to 2kW power requirement and up to 120kg*m² system moment of inertia.

Note: BST is currently in the development stage for several LEOS-100 missions.

CHARACTERISTICS

• System:
  • LEOS-100HR: 120kg class satellite
  • LEOS-100HP: 150kg class satellite
• Payload:
  • Volume: (HR/HP): 600x600x600mm³
  • Mass: (HR/HP): 50kg / 75kg
  • Power (HR/HP): average 60W/300W
    peak 300W/2kW
• Bus:
  • ADCS: 3-Axis stabilized
  • S-Band TTC
  • 320Mbit/s X-Band data
  • Electric Propulsion 100m/s dv
• Design Life: 5 Years

Please also have a look at our data sheet:

Data Sheet LEOS-100

• LEOS-50 Platform
• All
• ADIstar-700