Editing Ramjet (section)

==Flight speed==
Ramjets generally give little or no thrust below about half the [[speed of sound]], and they are inefficient ([[specific impulse]] of less than 600 seconds) until the airspeed exceeds {{convert|1000|km/h|m/s mph}} due to low compression ratios.

Even above the minimum speed, a wide [[flight envelope]] (range of flight conditions), such as low to high speeds and low to high altitudes, can force significant design compromises, and they tend to work best optimised for one designed speed and altitude (point designs). However, ramjets generally outperform gas turbine-based jet engine designs and work best at supersonic speeds (Mach 2–4).<ref>[http://web.mit.edu/16.unified/www/SPRING/propulsion/notes/node85.html#SECTION06363300000000000000 11.6 Performance of Jet Engines<!-- Bot generated title -->].</ref> Although inefficient at slower speeds, they are more fuel-efficient than rockets over their entire useful working range up to at least {{convert|6|Mach|m/s km/h|sigfig=2}}.

The performance of conventional ramjets falls off above Mach 6 due to dissociation and pressure loss caused by shock as the incoming air is slowed to subsonic velocities for combustion. In addition, the combustion chamber's inlet temperature increases to very high values, approaching the dissociation limit at some limiting Mach number.