Ram Accelerator

University of Washington


The ram accelerator is a novel launcher technology used to accelerate projectiles to hypersonic/hypervelocity speeds.  It is theoretically capable of accelerating projectiles to velocities greater than 8 km/sec (18,000 mph).  The device was developed in 1983 by researchers of the Department of Aeronautics and Astronautics at the University of Washington and operates similarly to a ramjet engine.  In the ram accelerator, a subcaliber projectile, shaped like the centerbody of a ramjet, is propelled down the center of a stationary tube that is filled with a premixed gaseous propellant.  As the projectile travels through the tube, the mixture is compressed, combusted, and expanded to produce thrust.  It has numerous applications that include researching hypersonic flows, missile defense systems, and cost effectively launching payloads into orbit around the earth.  More detailed information about the ram accelerator's history and various research topics are available on these pages and the links to related research sites.

[projectile.gif]  Layman's Description

  General Ram Info

  Technical Description

  UW Ram Accelerator Facility

  Ram Projectile Designs

  Research Topics

  Direct Space Launch Considerations

  History of Ram Accelerator Development – in progress

  Ram Accelerator Facilities From Around the World

  International Ram Accelerator Workshops – in progress

  Contact Ram Personnel

  Links to Related Facilities

  Ram Publications

  Ram Accelerator Patents

  Cartoons

  Ram Single Stage Movie (13MB)

 

 

You may also want to visit:

The University of Washington - Department of Aeronautics and Astronautics

The University of Washington

 


Please contact Dr. Carl Knowlen if you have any questions or comments.