
THRUSTERS
Non-Toxic 'Green' Chemical Propulsion Thrusters
Dawn's bi-propellant systems use nitrous oxide (N₂O) and propane (C₃H₆) to deliver reliable thrust without the handling risk, cost, and operational complexity of traditional toxic fuels such as hydrazine.
The B1 and B20 are both flight-ready 1 N and 20 N green propulsion thrusters designed to make spacecraft operations easier, from integration on the ground to reliable performance in orbit.
The success of Dawn's B1 and B20 have lead to the current in-development sized of the B5 (5 N) and B200 (200 N), becoming available later in 2026.
Benefits of Chemical Propulsion
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High thrust
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Lower power
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Modular
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Scalable - 30 kg to 500+ kg satellites
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LOOP refueling network capable
THRUSTERS
B20 Thruster - 20N
The B20 is a 20 N green chemical thruster designed for reliable, repeatable spacecraft propulsion, from ground testing through on-orbit operations. The B20 is ideal for larger orbit changes and delta-V missions of bigger 'small satellites' including Lunar and Deep space missions.
Overview:
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Higher thrust — supports orbit raising, and larger manoeuvres
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Integrated thruster, valves, and control electronics
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Additively manufactured Inconel 718 thruster body
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Health monitoring instrumentation
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Standard power and data interfaces for easy to command and operate.
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Operable under ambient conditions for fast ground testing
Heritage:
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100+ successfully launched into orbit

B20 Specifications
Performance
Thrust, range
6.46 to 18.11 N (1.45 to 4.07 lbf)
Minimum impulse bit
Bi-prop: 0.98 N.s (0.22 lbf.s)
Cold-gas: 10 mN.s (0.02 lbf.s)
Ignition
Spark-based igniter
Pulse frequency
4 Hz
Restarts
10,000+ per thruster
Physical
Thruster dimensions
176 x 80 x 79 mm
6.93 x 3.15 x 3.11 in
Dry mass
695 g (1.53 lbm)
Nozzle expansion ratio
100:1
Valves
Normally-closed solenoid
Four per thruster (firing and isolation)
Interfaces
Mounting
3x M5 threaded holes
Operations
Control
Operable together or independently
Select your desired quantity
Pair with B1 thrusters.
Firing modes
Bi-prop & cold-gas. Switch at will. Managed by not engaging the spark-ignitor.
Cold-start capable
Yes. Highly repeatable
THRUSTERS
B1 Thruster - 1N
Dawn's 1 N class thruster is designed for fine attitude control and small manoeuvres, particularly on CubeSats and small satellites. It is the core propulsion element in Dawn’s CubeDrive modules and can be used in clusters for full 6-axis control.
Overview:
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Low thrust, precision control — ideal for pointing, station-keeping, collision avoidance
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Integrated thruster, valves, and control electronics
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Additively manufactured Inconel 718 thruster body
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Standard power and data interfaces
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Operable under ambient conditions for fast ground testing
Heritage:
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50+ successfully launched into orbit on cubesat and small satellite

B1 Specifications
Performance
Thrust, range
0.49 to 1.35 N (0.11 to 0.30 lbf)
Minimum impulse bit
Bi-prop: 74 mN.s (0.016 lbf.s)
Cold-gas: 1.4 mN.s (3.1e-4 lbf.s)
Ignition
Spark-based igniter
Pulse frequency
4 Hz
Restarts
18,000+ per thruster
Physical
Thruster dimensions
108 x 79 x 40 mm
4.25 x 3.11 x 1.58 in
Dry mass
260 g
0.57 lbm
Nozzle expansion ratio
100:1
Valves
Normally-closed solenoid
Two per thruster
Interfaces
Mounting
4x 3.2mm holes.
Operations
Control
Operable together or independently
Select your desired quantity
Pair with B20 thrusters
Firing modes
Bi-prop & cold-gas. Switch at will. Managed by not engaging the spark-igniter
Cold-start capable
Yes. Highly repeatable




30+ customers across the globe, from the United States to France, India, Japan, Italy, Germany,
The Netherlands, South Korea and more.

SELF PRESSURIZING
Nitrous oxide (N₂O) and Propene (C₃H₆)

High Performance
Cold-start capable; 12,000+ restarts
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Pulse-mode capable
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Cold-gas mode
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Low power

Domestically available
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Fuel (C₃H₆)
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Oxidiser (N₂O)

Self-pressurized
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No separate pressurization system and no regulators

Less parts = more reliability
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Additively manufactured: fewer interfaces, fewer seals

Non-toxic
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Easy to handle
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Lower risk
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Ride-share friendly

Spark ignition
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No catalysts




