Ongoing-Project

SABATIER
FUEL PLANT

The quest to make fuel on Mars

THE IDEA

The unique atmospheric and geological features on Mars allow for in-situ production of methalox (liquid methane-liquid oxygen) propellant, which would make Mars return missions more feasible. Methalox is easier to handle and store compared to conventional liquid hydrogen propellant. For example, SpaceX has unveiled plans for a reusable launch vehicle, Starship, and the accompanying Mars mission architecture, which relies on in-situ propellant production to supply fuel for the trip back to Earth. Before such a system can be deployed on Mars, a feasibility study and rigorous tests at smaller scales must be conducted on Earth.

Details

The reactor core is where the actual reaction takes place and where methane is made. It is packed with either a ruthenium or nickel-based catalyst. There is a thermocouple to measure the temperature of the gases.

In the current design, the heating is provided by a coil of nichrome wire, tightly wound around the tube and sandwiched in between two layers of exhaust tape, encased in 5 inches of housing insulation on all sides. The highest temperature we ran it to was 700-degree Celsius.

The control system is responsible for regulating and reporting all operation values. This includes the temperature of the system, the valves, and the mass flow controllers.

The MFCs regulate the mass which passes through it. Each controller is calibrated to each of the gases which are passing through it. The maximum flow rate of the controller is 2L/min.

Project Timeline

August 2019
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November 2019
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August 2021
Tape Experiment
December 2021
February 2022
Tape Experiment

Dry run test

February 2022

June 2022
Tape Experiment
June 2022
Tape Experiment
Present day
Tape Experiment
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