LEOS-100

LEOS-100 image

Overview

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: 120 kg class satellite
- LEOS-100HP: 150 kg class satellite
Payload:
- Volume: (HR/HP): 600 x 600 x 600 m³
- Mass: (HR/HP): 50 kg / 75 kg
- Power (HR/HP): Average 60 W / 300 W
- Peak Power: 300 W / 2 kW
Bus:
- ADCS: 3-Axis stabilized
- S-Band TTC
- 320Mbit/s X-Band data
- Propulsion type: Electric Propulsion
- Delta-V Capability: 100 m/s
- Design Life: 5 Years

Specifications

Component Type
SmallSat Platform
Form Factor
SmallSat
Dry Mass
120.0 kg
Average Power
60.0 W
Heritage
N/A
Status
In Production
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