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