ELECTRIC PROPULSION SYSTEM
REGULUS-150-I2
A scale-up version of REGULUS-50
for the in-space mobility of micro- and minisatellites.
![regulus-150-t4i](https://www.t4innovation.com/wp-content/uploads/2022/02/regulus-150-t4i.png)
APPLICATIONS
REGULUS-150-I2 enables new mission scenarios and efficiently makes in-track maneuvers possible, compensates drag in VLEO and performs end-of-life operations.
![continuous-drag-compensation](https://www.t4innovation.com/wp-content/uploads/2021/03/continuous-drag-compensation.png)
CONTINUOUS DRAG COMPENSATION
![Altitude-changes](https://www.t4innovation.com/wp-content/uploads/2021/03/Altitude-changes.png)
ALTITUDE CHANGES
![decommissioning](https://www.t4innovation.com/wp-content/uploads/2021/03/decommissioning-1.png)
DECOMMISSIONING
![Phasing-Station-keeping](https://www.t4innovation.com/wp-content/uploads/2021/03/Phasing-Station-keeping.png)
PHASING
STATION KEEPING
![deorbiting](https://www.t4innovation.com/wp-content/uploads/2022/05/deorbiting.png)
DE-ORBITING
A propulsion system designed to be easily integrated into different satellites and to match customer’s requirements, with no customization efforts.
![regulus-150-t4i-thruster](https://www.t4innovation.com/wp-content/uploads/2022/02/regulus-150-t4i-thruster.png)
~3U
VOLUME
MICRO-
AND MINISATELLITES
I2
PROPELLANT
MAIN FEATURES
Thrust | 0.3 – 1.6 mN (highly modulable, 1.6 mN @ 150 W) |
Specific Impulse | Up to 720 s (@ 150 W) |
Input power | 50 – 150 W (150 W nominal) |
Mass flow | 0.2 – 0.35 mg/s |
Volume | 11 x 11 x 30 cm (tank excl.) |
Weight | 4.5 kg |
Electric Interface | 28±4 Vdc (24-32 Vdc) |
Communications | CSP over I2C or CANBUS and CSP over KISS-RS422 |