Dawn 22N Green Bi-Propellant Propulsion System

Utilising nitrous oxide and propene propellants in a self-pressurising configuration, Dawn's 22N propulsion system has increased capabilities compared to hydrazine, ADN or HAN-based systems. No PMD requirements or other complexities mean simple feed and tank designs.

Self-pressurising propellants mean one system for both in-orbit and re-entry operations. Stable pressure and mass flow rates give a constant Isp of >285N.s - throughout life. Unlike other green propellant thrusters that can take up to 30seconds to fire, Dawn's 22N requires no preheating of catalysts and is cold-start capable. Designed for both steady state and tiny pulse operations, the rapid cold-start capable boasts a minimum impulse bit of <4 N.s, allowing for the finest of manoeuvres.

Dawn can provide systems to suit any satellite. From thrusters only, through to complete tank, feed and health monitoring systems. We can scale up or scale down to suit your needs. REACH compliant and ITAR free, Dawn's 22N thruster is able to launch with all global launch services.

Specifications
Lead Time:
6 months
Type:
Propulsion
Nominal Thrust:
22N
Specific Impulse:
>285 s
Minimum Impulse Bit:
<4 N.s
Operational Temperature:
-5°C to 35°C
Dry Mass:
330 g
.:
Cold start capable. No preheating catalysts
.:
Self-pressurising propellants
Nominal Power Consumption:
12 W
Propellant Type:
Nitrous Oxide and Propene
Regulatory:
ITAR free and REACH compliant
.:
No propellant degradation over time
Documents