[AR] Re: L* for LOX/methane

  • From: "Doug Jones" <dmarc-noreply@xxxxxxxxxxxxx> (Redacted sender "randome" for DMARC)
  • To: arocket@xxxxxxxxxxxxx
  • Date: Fri, 23 Feb 2018 09:07:54 -0800

One of the keys to the 5M15's success was that the methane regen coolant was completely vaporized before reaching the injector, so that the gaseous methane provided lots of shear in the coax. We did have a low amplitude 12 Hz rumble, but connecting a modest volume accumulator through an orifice to the injector fuel plenum would have stopped that. We just didn't bother on that fast-paced program (we built a new test stand, test site, and two engines and ran all the tests -including bomb testing- between May 2006 and July 2007).

When we ran a very rich test point, the methane (LNG actually) Mdot was high enough relative to the heat flux that it did not completely vaporize, reaching the injector in two-phase flow... and the 12 Hz rumble went away completely because the speed of sound is so low in a foam that the Pc could not feed back to the fuel flow.

On 2018-02-22 4:39 PM, Henry Vanderbilt wrote:

GMTA!  LN2 is cheap and doesn't go bang; it's an obvious pre-chill for LCH4 plumbing.

But yeah, Murphy guarantees that bringing the bare minimum of any vital consumable to an important test will cause you to need more than you have.  (On a good day, that just means you ran out of caffeinated soda in the cooler.)

On that other matter, yes, I'm pretty sure having a propellant transitioning from liquid to gas an uncontrolled distance before the injector can couple chamber pressure back to the transition point and result in low frequency chamber pressure variations.  My I-was-only-a-manager-the-engineers-would-know-more guess is that once you get decent quality liquid to both fuel and LOX injectors, that sort of thing should settle down.

Henry

On 2/22/2018 5:04 PM, Carl Tedesco wrote:
We did have an LN2 chilldown procedure, but due to some holds/recycles, we
ran out of LN2 ☹ Will bring a full dewar next time.

Carl Tedesco

-----Original Message-----
From: arocket-bounce@xxxxxxxxxxxxx [mailto:arocket-bounce@xxxxxxxxxxxxx] On
Behalf Of Henry Vanderbilt
Sent: Thursday, February 22, 2018 2:38 PM
To: arocket@xxxxxxxxxxxxx
Subject: [AR] Re: L* for LOX/methane

Interesting issue there, RE keeping the injected propellant liquid from the
start in a LOX-methane motor intended to run liquid-liquid.

Yes, chilling down the LOX circuit before firing is routine for LOX-whatever
engines, but doing so for both propellant paths on a LOX-methane engine
could get WAY too exciting in terms of pad fires, hard starts, etc.

Maybe set up the LOX and methane circuits in good enough mechanical/thermal
contact so you can slowly pre-chill both with a trickle of LOX?

Or pre-chill the methane path with LN2 from a separate ground supply?

Henry

On 2/22/2018 3:26 PM, Carl Tedesco wrote:
Thanks Doug.  That's shorter than I expected.

If C* were less than 18" I assume C*_eff would start to drop off.
Would you expect combustion instability. I'm asking because a LOX/CH4
motor we hot-fired a few weeks ago had a low L* and had a significant
low-frequency sound and obvious "sputtering/chugging". It had co-axial
injectors which were intended to be liquid-liquid, but were likely
gas-gas (or low-quality liquid at best), since the plumbing may not
have reached thermal equilibrium.

--- Carl Tedesco









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