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posted by takyon on Saturday June 20 2015, @03:39PM   Printer-friendly
from the check-out-glasses-guy-in-the-header-image dept.

According to a press release from the European Space Agency (ESA), a team of scientists from Airbus have succesfully tested a prototype 10 N hydrazine thruster, its chamber and nozzle made out of a platinum–rhodium alloy, printed with "a laser machine normally employed for making jewellery, which is the current industrial state-of-the-art for manufacturing with these metals"

The world's first spacecraft thruster with a platinum combustion chamber and nozzle made by 3D printing has passed its baptism of fire with a series of firings lasting more than an hour and 618 ignitions.
"This is a world first," explains Steffen Beyer of Airbus Defence & Space, managing the project. "The firings included a single burn of 32 minutes, during which a maximum throat temperature of 1253°C was attained.

The main reason for 3D-printing was economical:

"Considering that platinum currently costs €40 a gram [sudo rm -rf: it seems to be more like 30€], 3D printing offers considerable future savings," added Dr Beyer. "We produce 150–200 thrusters in this class per year for different customers. 3D printing should allow shorter production cycles and a more flexible production flow, such as manufacturing on demand."


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  • (Score: 2) by kaszz on Saturday June 20 2015, @06:47PM

    by kaszz (4211) on Saturday June 20 2015, @06:47PM (#198767) Journal

    So Hydrazine + Iridium => exothermic reaction?

    What's LF2?

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  • (Score: 2) by gman003 on Saturday June 20 2015, @07:48PM

    by gman003 (4155) on Saturday June 20 2015, @07:48PM (#198782)

    Liquid elemental fluorine.

    At least in theory, the most efficient (highest specific impulse) chemical rocket you can make burns F2+H2=> 2 HF, with excess hydrogen. There's honestly not too much research into this anymore, it's too dangerous (as evidenced by the fact that the exhaust compound is pure hydrofluoric acid) and by the time you need that much efficiency, non-chemical rockets are better anyways. But related systems are investigated - fluorine compounds like ClF5 are perpetually on the verge of being used, or so the labs claim.

    And pure hydrazine honestly doesn't need much of an excuse to start an exothermic reaction. Iridium is just useful as a way to start a controlled burn, instead of "whoops the whole thing exploded again".

    • (Score: 2) by fritsd on Saturday June 20 2015, @08:25PM

      by fritsd (4586) on Saturday June 20 2015, @08:25PM (#198794) Journal

      Can they actually find researchers masochistic enough to want to work with liquid F2??!?

      I mean: pp mentioned fuming nitric acid, I once almost mutilated my hand with that stuff (not exactly, it was for nitration, so it was blended with fuming sulphuric acid).
      As my glove was beginning to smoke and turn black, I quickly turned the tap on and diluted it. (Remember kids: always wear your rubber gloves in the laboratory).

      I don't think anything can protect you if you come in contact with liquid F2. It seems a bit of a prestige project: "MY rocket uses a fuel that other rocket scientists and emergency services don't even dare to come near!!".
      And besides, what does the release of several tonnes of HF launched in the air do to the ozone layer?

      • (Score: 2) by kaszz on Saturday June 20 2015, @09:11PM

        by kaszz (4211) on Saturday June 20 2015, @09:11PM (#198800) Journal

        Use a robotic hand?

        The risk that is harder to avoid is the one any astronaut takes by riding on top of all that explosive stuff. Even if RP1+LOX isn't as bad as hydrazine. I don't it's a good idea to be soaked in it.

      • (Score: 3, Interesting) by gman003 on Saturday June 20 2015, @10:03PM

        by gman003 (4155) on Saturday June 20 2015, @10:03PM (#198812)

        Oh, there's people who would work with LF2, and worse.

        If you want a nice book to read on the topic, I suggest John Clark's "Ignition!".

        He was a rocket chemist, figuring out fuels and oxidizers in the 50s and 60s. He was one of the guys who figured out adding a pinch of hydrofluoric acid to red fuming nitric acid would prevent it from corroding aluminum or stainless steel.

        At one point, he was tasked with finding an extremely dense fuel, for use on missiles. Someone suggested to him dimethyl mercury as an additive. He actually tried running tests on it, but when he was unable to find anyone who would synthesize 100lbs of dimethyl mercury, he decided the whole idea was rather stupid (it would merely double density at best, while completely trashing all other performance figures and being unbelievably toxic). To demonstrate this absurdity, he wrote a proposal for an engine that injected straight mercury into the chamber. The theoretical math showed quite a nice improvement in impulse per volume by doing this, but he expected such a ludicrous proposal to be shot down instantly.

        Instead, the Navy told him to get to work testing it.

        Well, he at least managed to fob the job off on a different test lab, one located in the middle of the desert rather than New Jersey, but they did indeed fire a rocket using liquid mercury as an additive, spraying mercury vapor straight into the atmosphere.

        Rocket scientists don't give a shit.