<blockquote><font class="small">In reply to:</font><hr /><p>Scramjet is short for supersonic combustion ramjet. A ramjet will not ignite until sufficient air pressure is rammed into the intake. On ramjets this occurs around 300-400 mph. As the name implies, a supersonic combustion ramjet must go supersonic before ignition can occur. <p><hr /></p></p></blockquote><br /><br />Generally a ramjet is operational at the speed greater than the speed of sound (Mach 1), and scramjet starts around Mach 5 but a better performance is usually around Mach 6 or higher. <br /><br />If you ride the regular commercial airplanes, you'd notice its engines have "fan blades". The fan blades are used to "compress" air to a higher pressure so it can produce thrust (much like when you blow air into a baloon and then let it go). Also, if you ride in a car going about 50 mph and you roll down the window & stick your hand out of window, you'll feel a "ram" of air pushing against your hand. Well, that "ram-air" is much much stronger at 750 mph (equivalent speed of sound), so if you can design an inlet to capture & "shape" how the air flow goes into your engine without lossing much of its high pressure, then you could use the "natural" air pressure to power your engine instead of using fan blades. That's the principal of how a ramjet works. <br /><br />A ramjet will slow the captured air from supersonic to subsonic (below the speed of sound) by the time it reaches to its combustor, injet fuel, burn, and push out to the back with a nozzle. This is where one gets thrust as the exit gases pushes against the funnel shape nozzle forward. But at some air speed, mainly above Mach 5~6, there's too much pressure losses by slowing the incoming air down to below the speed of sound, making a ramjet less efficient. So the approach is to let the incoming air to stay supersonic as it enters the combustor, inject fuel, burn and pushes the gases back out of its nozzle. They called this "<font color="yellow">S</font> <div class="Discussion_UserSignature"> </div>