TEPCE: A Tethered Electrodynamic Propulsion CubeSat Experiment

Abstract

TEPCE was a 3U Cubesat that was developed to explore the feasibility of using electrodynamic propulsion for spacecraft. Propulsion is generated by conducting an electric current along a long wire, called a tether, that connects two spacecraft end-masses. As the spacecraft moves along its orbital path the Earth's magnetic field induces a Lorentz force between the magnetic field and the electrons in the tether which results in thrust for the spacecraft. It requires no chemical or other traditional fuel source. TEPCE was one of the first self contained electrodynamic propulsion spacecraft.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Feb 28, 2022
Accession Number
AD1161973

Entities

People

  • C L Enloe
  • Cameron Crippa
  • Gil Dutchover
  • Ivan Galysh
  • Joe Carroll
  • Matthew D. Brunner
  • Scott Kindl
  • Shannon Coffey
  • Zachery Sibert

Organizations

  • United States Naval Research Laboratory

Tags

Communities of Interest

  • Advanced Electronics
  • Energy and Power Technologies
  • Materials and Manufacturing Processes
  • Sensors
  • Space

DTIC Thesaurus Topics

  • Artificial Satellites
  • Attitude Control Systems
  • Charged Particles
  • Circuit Boards
  • Communication Systems
  • Computers
  • Control Systems
  • Detectors
  • Electromagnetic Fields
  • Electrons
  • Engineering
  • Field Effect Transistors
  • Graphical User Interface
  • Magnetic Fields
  • Operating Systems
  • Physics
  • Satellite Buses
  • Solar Cells
  • Solar Panels
  • Space Objects
  • Space Systems
  • Spacecraft

Fields of Study

  • Physics

Readers

  • Electrical Engineering
  • Plasma Physics / Magnetohydrodynamics
  • Space Exploration and Orbital Mechanics.

Technology Areas

  • Microelectronics
  • Space
  • Space - Hall-Effect Thruster
  • Space - Orbital Debris
  • Space - Satellites