- Type:
- Cubesat Propulsion
- Lead Time:
- 6 months
- Nominal Thrust:
- 0.5N
- Regulatory:
- ITAR free and REACH compliant
- Propellant Type:
- Nitrous oxide (N2O) and propene (C3H6)
- Specific Impulse:
- >285 s
- .:
- Cold start capable. No preheating catalysts
- Operating Temperature Range:
- 0°C to 30°C
- .:
- No propellant degradation over time
- Nominal Power Consumption:
- 12.5 W
- Minimum Impulse Bit:
- 35 mN.s
- Thrust Vector Control:
- 2-axis
- Delta-v:
- >230 m/s (for typical 3U CubeSat)
- .:
- No thruster degradation over time
- Maximum Impulse Bit:
- 7,500 mN.s
- Interface:
- PC/104
- Interface:
- RS485
- Radiation Tolerance:
- 50 krads
- Flow Rate:
- Oxidizer at 170 mg/s; Fuel at 18 mg/s
- Proof Pressure:
- Oxidizer at 110 bar; Fuel at 40 bar
- Burst Pressure:
- Oxidizer at >150 bar; Fuel at >55 bar
- Sensor(s):
- 1 temperature sensor; 2 pressure sensors