OUR TECHNOLOGY

Meet the thruster K-3: the secret sauce of our VLEO satellites.

Thruster technology

Our proprietary engine is an Air-Breathing Electric Propulsion system that collects atmospheric particles and converts them into plasma to generate continuous thrust.

Air-intake

The intake system captures atmospheric particles at altitudes between 150–400 km. Designed for maximum efficiency, it compresses the rarefied air by up to 100×, creating a stable flow for the thruster ionization. Image taken at VKI during a test campaign.

Plasma Thruster

The collected air is ionized into plasma and accelerated by our Helicon Plasma Thruster. This continuous propulsion counteracts aerodynamic drag, keeping satellites in stable Very Low Earth Orbits for +10 years. Image taken at IRS during a test campaign.

THE TRUE ENABLER OF VLEO MISSIONS.

Our K-3 thruster is designed for sustained operation in Very Low Earth Orbit. It delivers high efficiency and long lifetimes, even under the harsh near-atmospheric conditions, with ignition resilience no other thruster can match.
Specifications

Thruster Type

Helicon Plasma Thruster

Propellant

Atmospheric Air

Operational Orbit

150–300 km

Lifetime

+10 years

Perfecting the VLEO platform.

From early prototypes to the latest K-3 model, Kreios Space has advanced its VLEO technology through years of testing and iteration — each step improving performance, efficiency, and reliability.

2021
K-1 Thruster
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First helicon plasma thruster prototype developed and tested in laboratory conditions, validating ignition and plasma generation methods. Image taken at IRS.
2023
K-2 Thruster
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Second-generation prototype integrated with the intake system and tested in vacuum. Demonstrated stable operation and extended run time. Image taken at IRS.
2024
K-3 Thruster
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Third-generation model, proved with multiple gases (O₂, N₂, Ar, H₂), power levels, and mass flow rates. Highest Isp, efficiency, and thrust achieved.
2025
Flight Integration
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Development of the prototype that will be tested in-orbit. Preparation for the satellite integration and certification for the launch.

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