[AR] Re: {Spam?} Re: thinking big once more

  • From: Jonathan Goff <jongoff@xxxxxxxxx>
  • To: arocket@xxxxxxxxxxxxx
  • Date: Wed, 28 Sep 2016 18:49:45 -0600

Yes. Typo on my part 600-900 bar.

On Wed, Sep 28, 2016 at 6:30 PM, Troy Prideaux <troy@xxxxxxxxxxxxxxxxxxxxx>
wrote:

Typo Police intervention: that should be 600-900 Bar yeah?



Troy



*From:* arocket-bounce@xxxxxxxxxxxxx [mailto:arocket-bounce@xxxxxxxxxxxxx]
*On Behalf Of *Jonathan Goff
*Sent:* Thursday, 29 September 2016 10:22 AM
*To:* arocket@xxxxxxxxxxxxx
*Subject:* {Spam?} [AR] Re: thinking big once more



Alex,

If the chamber pressure of Raptor is 300bar / ~30MPa / ~4500psi, wouldn't
that imply a much higher high-side pressure for the oxygen and the fuel
component that goes into the preburner? I don't know what sort of multiple
of chamber pressure is typical for the pump outlet pressure on FFORSC
engines, but I had usually heard 2-3x, which would imply something closer
to 60-90 bar (9000-14000psi). Could someone who actually knows turbopumps
chime in?

Raptor's chamber pressure is 20-30% higher than most of the RD-170 family
engines.

~Jon





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