[AR] Re: Steel And rockets?

  • From: Henry Vanderbilt <hvanderbilt@xxxxxxxxxxxxxx>
  • To: arocket@xxxxxxxxxxxxx
  • Date: Wed, 21 Jul 2021 15:32:55 -0700

The EZ-Rocket engine development was before my time there.  Resolve an ambiguity for me?  Is that isopropyl/water or ethanol/water you mention as being tried and rejected before y'all settled on straight isopropyl?  (Or, both?)

On a historical note, the V-2 engine ran OK on a 75/25 ethanol/water mix, with a need for additional cooling often mentioned as one of the reasons.  You get more performance with less water, of course, as long as the engine doesn't fry.  (I just realized, XCOR experience is also "on a historical note" now :-(

Though there's another thing about ethanol - it's so massively hygroscopic that it's really hard NOT to have at least some water in the mix.

Anyway, I expect any further details you recall about alcohol/water mixes would be of interest here.

Henry

On 7/21/2021 2:04 PM, Doug Jones wrote:

Water alcohol mixes are much more viscous than either alone, and have poor mixing and energy release efficiency even at 90% alcohol. We tried it briefly at XCOR and went to straight IPA, never looked back.

On Wed, Jul 21, 2021, 1:19 PM Henry Vanderbilt <hvanderbilt@xxxxxxxxxxxxxx <mailto:hvanderbilt@xxxxxxxxxxxxxx>> wrote:

    Stop me if you've heard this already, but one regen-cooled
    incremental-testing trick available with ethanol fuel is to start
    out tests with a water-ethanol mix, for extra cooling.  Then once
    you have the engine operating, you can back off the water in the
    mix and work your way up toward your actual chamber cooling limits.

    Turning the problem around, you might design your chamber and
    cooling as best you can for your operating goals, then sneak up on
    those goals incrementally by beginning testing with more water in
    the fuel.  It is almost inevitable you'll be off in your initial
    cooling calculations, but this way you should get useful test
    experience and data with your first design pass at cooling design
    even if it turns out to be quite a bit off.

    Henry

    On 7/21/2021 12:44 PM, Charlie Jackson wrote:

    Okay, so if I were to attempt to use aluminium would it be better
    to increase the combustion chamber size to improve the effects of
    regenerative cooling? I intend to try water-cooling at first so
    I’d assume that is going to remove a lot of heat from the chamber
    in comparison to ethanol.

    *From: *Henry Spencer <mailto:hspencer@xxxxxxxxxxxxx>
    *Sent: *21 July 2021 19:32
    *To: *Arocket List <mailto:arocket@xxxxxxxxxxxxx>
    *Subject: *[AR] Re: Steel And rockets?

    On Wed, 21 Jul 2021, Charlie Jackson wrote:

    > ...I have noticed that they use steel for the combustion chamber

    > material...I understand that steel has a lower heat transfer rate

    > compared to copper but is it still viable?

    If you're using ablative, film, etc. cooling rather than
    regenerative

    cooling, then certainly -- and if you're trying for something
    small, bear

    in mind that regen cooling scales down poorly.  Even with regen
    cooling,

    yes, steel is viable, although it will be harder to make the cooling

    design work.  It's been done many times, especially in the early
    days.

    It has the advantage of being quite a bit stronger, which means
    you don't

    need as much of it.  The reason why the Big Boys seem to use
    rather weird

    copper alloys a lot is that plain copper isn't very strong, but
    anything

    added to make an alloy reduces conductivity.  So they're willing
    to use

    exotic alloying metals like zirconium, which give helpful strength

    improvements even in quite small amounts.  But those alloys
    aren't easily

    available to amateurs or startups.

    Remember that ordinary steel is brittle at LOX temperatures, and
    so isn't

    safe for anything that's going to be exposed to LOX, even
    briefly.  For a

    LOX engine, you'd want to make the injector and LOX plumbing out of

    something else, and think hard about transient exposures at
    startup or if

    something goes wrong (it will).

    A third option is aluminum -- light, highly conductive (not
    nearly as good

    as copper, but a lot better than steel), fine for LOX, mostly not
    grossly

    expensive.  You have to cool the bejesus out of it, because it loses

    strength very quickly as it warms up, but the high conductivity
    makes it

    more forgiving than steel.  It's an unusual choice but there are
    folks who

    swear by it.

    Particularly if you are trying for regen cooling, bear in mind
    that you

    will have to make more than one chamber.  You *won't* get it
    exactly right

    the first time, or the second, and getting it wrong tends to mean
    ruining

    the chamber.  A practical development project, especially a
    low-budget

    one, has to be able to tolerate failures:  "if failure is not an
    option,

    success can get expensive" (Peter Stibrany).  If making one
    chamber, or

    even two or three, is going to strain your budget, you're headed for

    disaster and should rethink your plans.  (And if *materials* look
    like a

    big part of your costs, you're probably being too optimistic
    about a lot

    of other costs.)

    Henry



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