After setting foot on the Moon, the next destination for humankind is Mars, which presents a whole new set of challenges in speedy, long-distance space travel.

  • anonionfinelyminced@kbin.social
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    7 months ago

    It’s a Rotating Detonation Rocket Engine"

    What makes the RDRE so revolutionary is that it makes use of a sustained detonation circling around a ring-shaped channel, fed by a mix of fuel and oxygen which is ignited by each passing explosion.
    Crucially, the RDRE uses less propellant fuel than conventional rocket engines, and is simpler in terms of its machinery and mechanisms. That means going into space becomes cheaper, and traveling further distances becomes possible.

    Saved you a click.

    • ramjambamalam@lemmy.ca
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      7 months ago

      NASA invented a space ship powered by a rotary engine? Noice, at least until the apex seals give out, but they should be good for 80k at least.

      • firecat@kbin.social
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        7 months ago

        No, it’s just gas powered car that still needs tanks and has everyone knows a around trip back to anywhere requires gas. The “ECO” of space travel.

          • firecat@kbin.social
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            7 months ago

            We don’t have unlimited fuel, rockets cost too much fuel. It’s not even normal fuel either, it’s rare chemistry rocket technology that takes a while to develop.

            • snugglesthefalse@sh.itjust.works
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              7 months ago

              Alright so nobody’s going to stop launching rockets realistically, there’s too much potential in space to just ignore, rdre are a way to do the same with less.

      • T156@lemmy.world
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        7 months ago

        Maybe the Jetsons, or the turbine engines in Star Wars? If you squint hard enough, it comes close enough.

  • Nighed@sffa.community
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    7 months ago

    This is a fancy aerospike engine right? The rotating detinations gives it higher chamber pressure and therefore better ISP or something?

    I will look for the Scott Manley video on this later (I think it was him?) Edit: also a Real Engineering one that explains the aero-spike nozzle

    Anyone have the ISP of this experiment to compare to other engines?