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  2. Prometheus Fuels - Wikipedia

    en.wikipedia.org/wiki/Prometheus_Fuels

    Prometheus Fuels is an American energy startup developing tools to filter atmospheric CO 2 using water, electricity, and nanotube membranes to produce commercially viable fuels. When powered by renewable electricity sources, e-fuels produced by such direct air capture methods do not contribute further emissions, making them carbon neutral . [ 1 ]

  3. Robert L. McGinnis - Wikipedia

    en.wikipedia.org/wiki/Robert_L._McGinnis

    Robert L. McGinnis is an American scientist, [1] technology entrepreneur, and inventor who has founded a number of technology companies including Prometheus Fuels, [2] Mattershift [3] and Oasys Water.

  4. Prometheus (rocket engine) - Wikipedia

    en.wikipedia.org/wiki/Prometheus_(rocket_engine)

    Prometheus is a backronym from the original French project designation PROMETHEE, standing for "Precursor Reusable Oxygen Methane cost Effective propulsion System", and for the Titan Prometheus, from Greek mythology, creator of humanity, and god of fire, known for giving fire to humanity in defiance of the gods.

  5. Direct air capture - Wikipedia

    en.wikipedia.org/wiki/Direct_air_capture

    This means that many DAC technologies are powered by fossil fuels, the very thing the technology is meant to eliminate reliance on. [35] The physical scale of the air contactor in any DAC system is a formidable challenge and may also have an impact on the environment.

  6. Reaction engine - Wikipedia

    en.wikipedia.org/wiki/Reaction_engine

    If the energy is produced by the mass itself, as in a chemical rocket, the fuel value has to be /, where for the fuel value also the mass of the oxidizer has to be taken into account. A typical value is = 4.5 km/s, corresponding to a fuel value of 10.1 MJ/kg. The actual fuel value is higher, but much of the energy is lost as waste heat in the ...

  7. Cryogenic rocket engine - Wikipedia

    en.wikipedia.org/wiki/Cryogenic_rocket_engine

    RL-10 is an early example of cryogenic rocket engine.. Rocket engines need high mass flow rates of both oxidizer and fuel to generate useful thrust. Oxygen, the simplest and most common oxidizer, is in the gas phase at standard temperature and pressure, as is hydrogen, the simplest fuel.

  8. AOL Mail

    mail.aol.com/?rp=webmail-std/en-us/basic

    Get AOL Mail for FREE! Manage your email like never before with travel, photo & document views. Personalize your inbox with themes & tabs. You've Got Mail!

  9. RD-8 - Wikipedia

    en.wikipedia.org/wiki/RD-8

    The RD-8 (Russian: РД-8 and GRAU Index: 11D513) is a Soviet / Ukrainian liquid propellant rocket engine burning LOX and RG-1 (a rocket grade kerosene) in an oxidizer rich staged combustion cycle.