Aerospace Garage

PRODUCT PROFILE

Arka Green Propulsion

SMALL SATELLITE PROPULSION

Arka Green Propulsion

New Zealand · verified

MAKER

Dawn Aerospace →dawnaerospace.comlast verified 6 Sept 2026
COUNTRY
New Zealand
PROGRAMME STATUS
verified

Specifications

Function
Provides orbital manoeuvres, station-keeping, and reaction control for small to medium satellites.
Platform fit
The modular architecture is designed to scale from 3U CubeSats up to 500kg class satellites.
Commercial model
Hardware is typically sold as a capital purchase, with optional engineering services for mission-specific tank sizing and integration support.
Deployment status
The system is flight-proven with multiple units currently operational in low Earth orbit.
Evidence to demand
Selection by various commercial constellation operators and space logistics companies indicates a growing shift toward green propellants.

Description

The Arka Green Propulsion system is a high-performance chemical thruster series developed by Dawn Aerospace as an alternative to traditional hydrazine-based systems. It utilizes a proprietary non-toxic propellant combination, primarily nitrous oxide and a fuel blend, which allows for simplified handling and lower ground support costs. The technology stems from the manufacturer's experience in building launch vehicles and satellite sub-systems, aiming to provide a 'turnkey' propulsion solution for the small satellite market. This system is sold both as a standalone thruster unit and as part of a fully integrated propulsion module, including tanks and control electronics. It is marketed toward commercial satellite operators and government space agencies seeking to comply with tightening environmental regulations regarding hazardous materials. The hardware is currently in active service, having been selected for various CubeSat and SmallSat missions, including those for commercial Earth observation and technology demonstration constellations. Potential buyers should evaluate the specific impulse trade-offs when switching from monopropellant hydrazine to this nitrous-based architecture. The Aerospace Garage desk would seek to verify the cumulative on-orbit firing hours across the different thruster sizes (ranging from 0.5N to 20N) to confirm long-term catalyst stability. We would also scrutinise the thermal management requirements, as nitrous-based systems can have different heat profiles compared to legacy toxic propellants.

Linked stories

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LAST VERIFIED

6 Sept 2026

SOURCE CITATION

Maker website on record

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