Payload capacity: 35 cm³ and 100 grams at 0.33 units
Unique features: fully redundant design, attitude control using magnetorquers, orbit determination using GNSS receivers, corner-cube reflectors for laser ranging from ground, communication (downlink) up to 2 Mbit/s
Possible applications: internet of things (IoT), on-orbit verification (OOV)
Unique features: redundant design, attitude control using reaction wheels, orbit determination using GNSS receivers, corner-cube reflectors for laser ranging from ground, communication up to 2 Mbit/s
Possible applications: internet of things (IoT), Earth observation (VIS) at 30 metres ground sampling distance, on-orbit verification (OOV)
2 to 3 Units
Credit: TU Berlin
Credit: TU Berlin
Design based on developments of NanoFF project at TU Berlin
Payload capacity: 1700 cm³ and 3 kg
Unique features: redundant design, attitude control using reaction wheels, orbit determination using GNSS receivers, propulsion system for orbit control, corner-cube reflectors for laser ranging from ground, communications with 4 Mbit/s
Possible applications: multispectral Earth observation (30 metres GSD at VIS channels, 90 metres GSD at TIR channel), on-orbit verification (OOV)
6 Units or Customized
Credit: TU Berlin
Design based on developments of SALSAT project at TU Berlin
Payload capacity: 4U and 8 kg
Total mass: up to 12 kg
Unique features: redundant design, attitude control using reaction wheels, orbit determination using GNSS receivers, propulsion system for orbit control, corner-cube reflectors for laser ranging from ground, communications with up to 100 Mbit/s
Possible applications: hyperspectral Earth observation, on-orbit verification (OOV), robotic applications
