Tiny Water-Powered Nano Rocket Thruster Designed to Fit on a Fingertip

 Imperial College's Innovative ICE-Cube Thruster: A Green and Efficient Water-Powered Propulsion System for Small Satellites

Tiny Water-Powered Nano Rocket Thruster Designed to Fit on a Fingertip
Tiny Water-Powered Nano Rocket Thruster Designed to Fit on a Fingertip


A group of scientists hailing from Imperial College London has unveiled a groundbreaking miniature rocket engine capable of operating on water, presenting a promising solution for maneuvering small satellites in the vast expanse of space.

This revolutionary propulsion system, christened the Iridium Catalysed Electrolysis CubeSat Thruster (ICE-Cube Thruster), derives its power from the principle of electrolysis—a process that dissects water into its constituent elements, hydrogen and oxygen, through the application of an electrical current.

At its core, the ICE-Cube Thruster features a remarkably efficient electrolyzer, demanding a mere 20 watts of electric power. This electrolyzer instigates the transformation of water into hydrogen and oxygen gases, which subsequently serve as the engine's propellant. These gases are then directed into a combustion chamber and nozzle, both compactly sized at less than 1mm, effectively generating the necessary thrust. By eliminating the necessity for bulky storage tanks to house gaseous propellants, a frequent obstacle in miniaturizing propulsion systems, the ICE-Cube Thruster significantly streamlines satellite design.

This cutting-edge engine is tailor-made for the burgeoning small satellite market, primarily composed of nanosatellites weighing less than 10 kg. These diminutive satellites are burdened by stringent constraints encompassing size, weight, power, and propellant, making the integration of conventional propulsion systems an arduous task.

Statistics reveal a projected tripling in the annual deployment of spacecraft since 2016, with nanosatellites, weighing under 22 lbs (10 kg), accounting for roughly 90% of spacecraft launches in 2017. These miniaturized satellites place heightened demands on propulsion systems, necessitating compactness, low power consumption, and eco-friendly propellants—requirements aptly met by the ICE-Cube Thruster.

This innovative propulsion system boasts several distinct advantages over its counterparts. Firstly, it employs water as a propellant, a substance known for its non-toxic, easily stored, and widely accessible properties. Secondly, it achieves remarkable performance, as hydrogen and oxygen rank among the most efficient chemical propellants available. Thirdly, its power requirements are a mere fraction of comparable electric propulsion devices, well-suited for the power constraints of nano-satellites. Lastly, it can be fabricated using micro-electronics techniques, ensuring high precision, scalability, and cost-efficiency.

What sets the ICE-Cube Thruster apart is its manufacturing process, which leverages micro-electrical mechanical systems (MEMS), a technique commonly employed in the microelectronics industry. This innovative approach enables the assembly of thruster components with sub-micrometer precision, enabling scalability and cost-effective batch production.

The ICE-Cube Thruster emerged as part of the ESA's General Support Technology Program (GSTP), aimed at mitigating the risks associated with new space technologies. During rigorous testing at Imperial College London, this miniature marvel demonstrated the ability to generate 1.25 millinewtons of thrust with a specific impulse of 185 seconds, on a sustained basis.

To provide context, this thrust is approximately half a billion times less than that harnessed by the iconic Space Shuttle engines. However, its diminutive size and impressive efficiency position it as a transformative invention for the CubeSat industry.

The data gathered during these experiments will serve as a compass for advancing the propulsion system towards a flight-ready model, including the electrolyzer. This development endeavor will be spearheaded by URA Thrusters in collaboration with Imperial College London.

The ICE-Cube Thruster stands as a micro-scale counterpart to the ICE-200 Thruster, a higher-thrust (1N) variant also conceived at Imperial College London. The ICE-200 Thruster operates on the same water electrolysis and iridium catalysis principle but features a larger combustion chamber and nozzle.

The ICE-200 Thruster has garnered recognition from ESA, being selected for deployment in the Lunar Pathfinder mission scheduled for 2024. This thruster will play a pivotal role in providing attitude control and orbit maintenance for the Lunar Pathfinder spacecraft.

Both the ICE-Cube and ICE-200 thrusters exemplify how water can serve as an environmentally friendly and efficient propellant for space missions. The researchers behind these innovations hold the optimistic outlook that their technology will pave the way for new applications and capabilities in the realm of small satellite exploration.

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