Metallic Induction Reaction Engine.

Abstract

Advances in electrical propulsion technology have inspired a variety of approaches for orbit raising propulsion. One such technique, the metallic induction reaction engine, uses a solid metallic reaction mass rather than a gas or plasma to achieve high thrust density and efficiency. The reaction mass is inductively accelerated by a magnetic pulse coil, thereby eliminating the problems of erosion and wear. The basic mechanisms and limits of the conversion of electrical energy into kinetic energy by the metallic induction reaction engine are analyzed. To facilitate this, a single shot experimental engine was constructed and operated over one hundred times, including several tests with conversion efficiencies greater than 50%. Further analyses were performed by developing a numerical model. The velocity and current predicted by this model agree to within 15% of the experimental data over the entire range of operation. Extrapolation to higher performance operation has revealed that there are adverse coupling effects and circuit impedance effects which can limit the ultimate performance of the metallic induction reaction engine.

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Document Details

Document Type
Technical Report
Publication Date
Dec 28, 1984
Accession Number
ADA160137

Entities

People

  • D. P. Hart
  • P. P. Mongeau

Tags

Communities of Interest

  • Advanced Electronics
  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Dielectrics
  • Differential Equations
  • Electric Power
  • Electric Propulsion
  • Energy
  • Energy Transfer
  • Heat Energy
  • Mechanical Engineering
  • Mechanics
  • Optical Detectors
  • Power Supplies
  • Propulsion Systems
  • Pulsed Power
  • Tensile Strength
  • Thermal Properties
  • Thermodynamics

Fields of Study

  • Physics

Readers

  • Combustion science or combustion engineering.
  • Pulsed Power and Plasma Physics.
  • Systems Analysis and Design

Technology Areas

  • Space
  • Space - Hall-Effect Thruster