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Dam Mars Study: Large Scale ISRU Propellant Production
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Description
Investigate the feasibility and risks of producing ISRU propellant for large-scale Mars ascent vehicles using hydroelectric power from the Martian ice caps. For this concept, flow channels will be created with components printed from regolith and fluid from sub-glacial lakes will flow thru printed turbines to produce the required power output.
Benefits
Explores a new opportunity for Martian propellant production at a scale that is required for human missions using chemical propulsion. This option avoids challenges faced by powering ISRU production using a fission or photovoltaic source by utilizing pressurized pools of liquid under the Martian glaciers to drive hydroelectric power. Such concepts have been studied and even implemented terrestrially, but this project will be the first to study the concept for Mars.
Details
| Technology area | Exploration Destination Systems > In Situ Resource Use > Resource Processing for Production of Mission Consumables |
| Program | Agency Independent Research and Development (A-IRAD) |
| Lead organization | Johnson Space Center, Houston, TX |
| Start date | 2025-11-01 |
| End date | 2026-09-30 |
Project contacts
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How to get involved
This is a mature technology (TRL 7+) — the realistic path in is usually NASA's Technology Transfer Program: licensing an existing NASA patent, or a Space Act Agreement to use NASA facilities/expertise directly. NASA also runs a startup licensing program with no upfront fee for companies formed to commercialize a specific NASA technology.
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