>
Three Bob Ross Paintings Sold for $600,000 at Auction in Fundraiser for Public Television
New Gel Regrows Dental Enamel–Which Humans Cannot Do–and Could Revolutionize Tooth Care
Delta Airlines Treats Teens to Free 'Dream Flights' Inspiring Many to Become Pilots and Engi
"Every reserve currency has COLLAPSED, the US dollar is next" We better buckle up!
Blue Origin New Glenn 2 Next Launch and How Many Launches in 2026 and 2027
China's thorium reactor aims to fuse power and parity
Ancient way to create penicillin, a medicine from ancient era
Goodbye, Cavities? Scientists Just Found a Way to Regrow Tooth Enamel
Scientists Say They've Figured Out How to Transcribe Your Thoughts From an MRI Scan
SanDisk stuffed 1 TB of storage into the smallest Type-C thumb drive ever
Calling Dr. Grok. Can AI Do Better than Your Primary Physician?
HUGE 32kWh LiFePO4 DIY Battery w/ 628Ah Cells! 90 Minute Build
What Has Bitcoin Become 17 Years After Satoshi Nakamoto Published The Whitepaper?

Georgia Tech aims to reduce the Entry Descent Landing (EDL) mass of a crewed mission to Mars by approximately 7 tons. This technology will enable long-term human presence on Mars and beyond because costly propellant deliveries from Earth would be unnecessary. They will genetically engineer algae to efficiently convert the abundant CO2 in the Martian atmosphere into liquid hydrocarbons suitable for rocket propulsion and other energy needs on Mars. The proposed system grows algae biofilms that consume atmospheric CO2 and sunlight with minimal water resources.
The algae then provide a food source to the genetically optimized organisms/microbes, which are engineered to produce a monomer with ideal combustion behavior and liquid properties. These monomers would be used in a pump-fed LOX/monomer propellant combination to power a human-crewed Mars Ascent Vehicle (MAV). They will focus on the production of C3-C4 diols, which have low melting points (less than -36ÂșC) for use as a liquid on Mars, and optimal energy content (over 14MJ/L), to provide the minimum thrust needed for ascent from Mars.
The chemical and physical properties, and energy density of these monomers suggest that they are capable of sufficient energy conversion through combustion for a crewed launch from Mars, making them excellent candidates for an ISRU rocket propellant. They are also liquid over a wide range of typical Mars temperatures, making them non-cyrogenic and storage stable. The oxygen atoms in the designed monomer will also enable a cleaner burn than conventional hydrocarbon propellants, supporting the reuse of rocket engines for multimission and interplanetary trips. Our approach will test the thermo-physical-chemical properties and combustion behavior of a suite of monomer rocket propellant candidates, while simultaneously developing the biological system for synthesizing them on Mars. By working together and in parallel, we will efficiently integrate testing feedback to quickly arrive at a co-optimized ISRU LOX/monomer rocket propellant. In total, these advantages will reduce infrastructure and resources needed to support human missions to Mars, and future, more ambitious efforts to expand human presence throughout the solar system.