[net.space] Scramjet problems

jcp@BRL-TGR.ARPA (07/05/84)

From:      Joe Pistritto <jcp@BRL-TGR.ARPA>

	Assuming that you could maintain a population of free radicals
thru means other than heating due to combustion, (Lasar dissociation was
postulated), you also have to worry about the kinetic energy of the
molecules being high enough to support the reaction.
	The SR-71A gets around this, (it has subsonic chamber flow, buts
its the same idea from a kinetic energy standpoint), by using the movable
shock cones on the front of the intakes to propagate a compression shock
wave INTO the intake, thereby raising both pressure and temperature.  Remember
also that the SR-71 operates at in excess of Mach 3.0, and the combustion
chamber flow NEVER goes Transonic.  It may be possible to maintain this,
(albeit at higher altitudes), for considerably higher Mach numbers...

	If you go high enough though, you run out of oxygen, which is another
story...

						-JCP-