An Exploratory Study of Ram Accelerator Principles

Abstract

A new method for accelerating projectiles from velocities of 0.7 km/ sec up to 12 km/sec using chemical energy is described. The concept, called the ram accelerator, is based on gasdynamic principles similar to those of a supersonic airbreathing ramjet but operates in a different manner. The projectile resembles the center body of a ramjet and travels through a tube filled with a premixed gaseous fuel and oxidizer mixture. The tube acts as the outer cowling of the ramjet and the combustion process travels with the projectile. By tailoring the propellant mixture along the tube, a nearly constant acceleration can be achieved. In principle, the ram accelerator is scalable for projectile masses ranging from grams to thousands of kilograms and is capable of ballistic efficiencies as high as 30 percent. Two theoretical models developed for analytical studies are described, one involving a simple quasi-steady, one-dimensional approach, and the other a computational fluid dynamic approach.

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1988
Accession Number
ADA202185

Entities

People

  • A. Hertzberg
  • A. P. Bruckner
  • D. W. Bogdanoff

Organizations

  • University of Washington

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Boundary Layer
  • Bow Shock
  • Chemical Reactions
  • Combustion
  • Combustion Products
  • Computational Fluid Dynamics
  • Computational Science
  • Efficiency
  • Fluid Dynamics
  • Fluid Mechanics
  • Heat Transfer
  • Ideal Gas Law
  • Plastic Explosives
  • Propellants
  • Turbulent Mixing
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Electrical Engineering

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow