[AR] Re: Ozone layer was Re: Removing Coking Deposits

  • From: Peter Fairbrother <zenadsl6186@xxxxxxxxx>
  • To: arocket@xxxxxxxxxxxxx
  • Date: Tue, 27 Sep 2016 11:20:40 +0100

On 27/09/16 03:39, Henry Spencer wrote:

On Wed, 21 Sep 2016, Peter Fairbrother wrote:
And wrong about that. Oh dear.
Is there no hope for horizontalists?

Perhaps some faint hope. :-)  There are some advantages to be had there,
even though they are often overstated.

I hope you haven't joined the SSTO club though :)

I hate to disappoint you, but I'm a lifetime member. :-)

Oh dear -perhaps you might explain?

Indeed, "very poorly populated" is probably an understatement.  Mach 6
at 100km is beyond anything ever done with a WWJ.  Even the X-15
couldn't do that (either one, but not both simultaneously).

One saving grace, perhaps - it's not a Mach 6 aircraft. By the time it
reaches ~ Mach 4 it's operating as a pure rocket, in near-vacuum.

Helpful though that is in some ways, it's a disadvantage in others.  In
particular, I think it means you'll need rocket thrust vectoring (or a
very hefty RCS) for control.  I don't think that's ever been done in a
rocket aircraft before; the X-15 high-altitude flights were all
ballistic trajectories, with the noisy flamey part :-) finishing at much
lower altitude where aerodynamic controls still worked.  Nothing
fundamentally hard about it, but it's another design complication (and
potentially a heavy one).

Didn't the X-15 have a HTP RCS? Perhaps they didn't use it for high altitude flights, though I can't think why.

-- Peter Fairbrother

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