[AR] Re: DARPA responsive launch challenge

  • From: John Schilling <john.schilling@xxxxxxxxxxxxxx>
  • To: arocket@xxxxxxxxxxxxx
  • Date: Sun, 22 Apr 2018 15:52:30 -0700

On 4/22/2018 3:38 PM, Henry Vanderbilt wrote:

On 4/22/2018 1:26 PM, John Schilling wrote:
It's just that, once you ignite the stuff in the chamber, it gets real enthusiastic about passing the word to its still-chill friends about this hot new "fire" stuff and convinces them to try it out before they've reached the proper venue.  I don't think we ever measured a critical diameter.

Well-behaved until it meets a significant ignition source, then everything with physical continuity to the ignition point undergoes a deflagration-to-detonation transition.  We had some ideas on how to approach that, but nothing that would meet cost and schedule and nothing we were going to submit an F-15 crew to.

Get the fluid velocity in the injector higher than the detonation-front velocity?

Sorry, bad joke, couldn't resist...

"And in step three, we show that achieving FTL speeds in the injection manifold allows the safe and practical use of a monopropellant with 320 seconds of specific impulse, thus revolutionizing space travel!"

        John Schilling
        john.schilling@xxxxxxxxxxxxxx
        (661) 718-0955

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