A ram accelerator is a device for accelerating projectiles to extremely high speeds using jet-engine-like propulsion cycles based on ramjet and/or scramjet combustion processes. It is thought to be possible to achieve non-rocket spacelaunch with this technology.
They consist of a long tube (barrel) filled with a mixture of combustible gases with a frangible diaphragm at either end to contain the gases. The projectile, which is shaped like a ramjet core, is fired by another means (e.g., a light gas gun) supersonically through the first diaphragm into the tube. It then burns the gases as fuel, accelerating down the tube under jet propulsion. Other physics come into play at higher velocities.
In a normal ramjet, air is compressed between a spike-shaped centerbody and an outer cowling, fuel is added and burned, and high speed exhaust gases are expanded supersonically out the nozzle to generate thrust. In a ram accelerator, a projectile having a shape similar to the ramjet centerbody is fired, (often from a conventional gun), into the accelerator barrel, causing compression between the projectile and the barrel's walls. The barrel contains a pre-mixed gaseous fuel-air mixture. As the ram accelerator projectile compresses the fuel-air mixture, it is ignited and the combustion is stabilized at the base of the projectile. The resulting pressure differential generates a prodigious amount of thrust that can accelerate projectiles to in-tube Mach numbers greater than 8. Thus, if propellant mixtures with a speed of sound of 1000 m/s (e.g. fuel-rich H2-O2 mixtures) are used, muzzle velocities in excess of 8000 m/s are possible.
To span a wide range in a typical ram accelerator system, multiple stages with propellants with different sound speeds are used to maintain high performance. Membranes or diaphragms that are easily punctured by the projectile are used to isolate the propellant stages. Each section is filled with a different fuel-air mixture chosen so that later sections have higher speeds of sound. As such, the ram can be maintained at optimal speeds of Mach 3–5 (relative to the mixture that it travels through) during its entire acceleration period. Ram accelerators optimized to use supersonic combustion modes can generate even higher velocities (Mach 6-8) due to the ability to combust fuel that is still moving at supersonic speed.
The chief advantage of a ram accelerator over a conventional gun is its scalability. In a normal gun, maximum pressure is exerted at the time of the initial charge detonation. As the projectile moves further down the barrel, the amount of acceleration upon the projectile decreases as the gas behind it expands, eventually reaching amounts trivial enough that a longer barrel is no longer justified (see internal ballistics). With a ram accelerator, the projectile is propelled primarily by the pressure generated by the reaction of the propellant gases burning just behind the projectile. This leads to constant pressure being put both on the gun and the projectile itself. Consequently, far longer barrels are possible than conventional guns, while still delivering a strong constant acceleration to the projectile.
Ram accelerators have been proposed as a cheap method to get payloads into space. Impulsive launched projectiles need some means to circularize their trajectory for orbit insertion, so rockets, such as those designed in Project HARP, are typically incorporated into the projectiles. Using rockets for upper stages, it is believed that a launch cost of less than $500 (US dollars, 2004) per kilogram can be attained. Using a tether or space tug would further reduce launch costs.
The main competitors to a ram accelerator for direct space launch applications are two-stage gas guns (SHARP), multiple sidewall injection gas guns (JVL), railguns and coilguns. Ram accelerators are currently used primarily for research into supersonic combustion. The scram cannon science fiction weapon was inspired by ram accelerators.
As of July 2007, the Ballistic Flight Group has been promoting commercial investment into the ram accelerator technology.
- The Ballistic Flight Group website
- accelerator home page (archive.org link) at the University of Washington.
- Detailed description (archive.org link) of ram accelerator operating modes (from the University of Washington page set).
- Pope, Gregory T. (March 1, 1994), "Ramming Speed", Discover Magazine, retrieved 2009-02-13