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Our rideshare-first design allows for flexible mission design.


Launched to LEO as any other satellite rideshare, providing unprecedented mission cadence.
PAYLOAD
20kg
TRANSIT TIME
4 months


| Propellant | HTP + RP-1 |
| Thrust | 500 N |
| Chamber Pressure | 10 bar |
| Isp | 311 s |
| Feed System | Electric Pump |