B1 Green Bipropellant Thruster
Flight-proven 1 N green bipropellant thruster using non-toxic N2O/propene, with dual bi-prop and cold-gas modes, 18,000+ restarts, and 50+ orbital flight heritage.
Technical specifications
- Thrust Range
- 0.49-1.35 N
- Propellant
- N2O + propene (C3H6) - non-toxic green
- Min Impulse Bit (bi-prop)
- 74 mNs
- Min Impulse Bit (cold-gas)
- 1.4 mNs
- Pulse Frequency
- 4 Hz
- Restarts
- 18,000+
- Dry Mass
- 260 g
- Dimensions
- 108 x 79 x 40 mm
- Nozzle Expansion Ratio
- 100:1
- Flight Heritage
- 50+ orbital flights
About
The Dawn Aerospace B1 is a flight-proven 1 N green bipropellant thruster using non-toxic nitrous oxide (N2O) and propene (C3H6) propellants. Operates in both bipropellant mode (74 mNs min impulse bit) and cold-gas mode (1.4 mNs min impulse bit) via spark igniter control. Supports up to 4 Hz pulse frequency and 18,000+ restarts. Launched on 50+ satellites in CubeSat and small satellite configurations. 100:1 nozzle expansion ratio.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.