Charleston
July 13th 03, 04:22 AM
"Al Jackson" > wrote in message
om...
> "Terrence Daniels" > wrote in
message k.net>...
> > About six or seven seconds before SRB sep (by my rough count) the
exhaust
> > plumes from the SRB's suddenly get very large and very bright. What's
> > happening there? Is it something to do with how the fuel is distributed
> > inside the case?
We do know that the exhaust plume expands as the vehicle goes from sea level
to a near vacuum at 140K feet, but that does not explain the phenomenon you
are talking about.
> The SRB rocket nozzles are recessed, thus Aluminum* Oxide pools near
> them when the motors are operating. When the pressure tails off in the
> solid rocket motors the liquid Aluminum Oxide boils violently. What
> you see are bright globs and shards of Aluminum Oxide being coughed
> out of the nozzle. Of course none of this gets into orbit!
> (One notes that Aluminum is mixed into the solid rocket motor fuel for
> energetic purposes.)
The aluminum is in very fine powder form and it *is* the fuel. It is
oxidized by very fine ammonium perchlorate to form alpha aluminum oxide.
This occurs at high temperatures around 5,900º F, IIRC. I am trying to
envision how oxides of aluminum which are by definition fumes, become a
boiling liquid. Are you saying that they are trapped, condense, and form
slag to some extent at the nozzle exit? Why would they cough at lower
thrust values? Could it be the transition from steady state combustion to
unsteady combustion or even a transition from supersonic velocity to
subsonic velocity during thrust tail-off? I always thought the bright chunks
were just isolated pieces of propellant along the case walls being ejected.
Daniel
om...
> "Terrence Daniels" > wrote in
message k.net>...
> > About six or seven seconds before SRB sep (by my rough count) the
exhaust
> > plumes from the SRB's suddenly get very large and very bright. What's
> > happening there? Is it something to do with how the fuel is distributed
> > inside the case?
We do know that the exhaust plume expands as the vehicle goes from sea level
to a near vacuum at 140K feet, but that does not explain the phenomenon you
are talking about.
> The SRB rocket nozzles are recessed, thus Aluminum* Oxide pools near
> them when the motors are operating. When the pressure tails off in the
> solid rocket motors the liquid Aluminum Oxide boils violently. What
> you see are bright globs and shards of Aluminum Oxide being coughed
> out of the nozzle. Of course none of this gets into orbit!
> (One notes that Aluminum is mixed into the solid rocket motor fuel for
> energetic purposes.)
The aluminum is in very fine powder form and it *is* the fuel. It is
oxidized by very fine ammonium perchlorate to form alpha aluminum oxide.
This occurs at high temperatures around 5,900º F, IIRC. I am trying to
envision how oxides of aluminum which are by definition fumes, become a
boiling liquid. Are you saying that they are trapped, condense, and form
slag to some extent at the nozzle exit? Why would they cough at lower
thrust values? Could it be the transition from steady state combustion to
unsteady combustion or even a transition from supersonic velocity to
subsonic velocity during thrust tail-off? I always thought the bright chunks
were just isolated pieces of propellant along the case walls being ejected.
Daniel