EPSS C1
EPSS C1
EPSS C1
1 Thruster
Thrust: 1N BOL to 0.22N EOL
Populsion System Power Monitoring: .19W
Propulsion System Power Preheat: 9.6W
Propulsion System Power Firing: 1.7W
Rad Tolerance: 20kRad
Mission Design Pressure: 25 to 4.7 Bar
Total Impulse: from 400 Ns
Thrust: 1N BOL to 0.22N EOL
Populsion System Power Monitoring: .19W
Propulsion System Power Preheat: 9.6W
Propulsion System Power Firing: 1.7W
Rad Tolerance: 20kRad
Mission Design Pressure: 25 to 4.7 Bar
Total Impulse: from 400 Ns
NanoAvionics
Cold-Gas Propulsion
CubeSat Propulsion System EPSS
Dry Mass: 1kg Wet Mass: 1.2kg
1.3U
CubeSat Propulsion EPSS C1 (1U) 2019.04.01 M6P
First in-orbit test performed during LituanicaSAT-2 mission