Inventors:
Ralph J. Zavesky - Parma OH
James S. Sovey - Strongsville OH
Michael J. Mirtich - North Olmsted OH
Charalampus Marinos - Middleburg Hts. OH
Paul F. Penko - Berea OH
Assignee:
The United States of America as represented by the Administrator of the
National Aeronautics and Space Administration - Washington DC
International Classification:
H05B 700
Abstract:
An electrothermal thruster utilizes a generally cylindrical heat exchanger chamber. A textured, high emissivity heater element radiatively transfers heat to the inner wall of this chamber that is ion beam morphologically controlled for high absorptivity. This, in turn, raises the temperature of a porous heat exchanger material in an annular chamber surrounding the cylindrical chamber. Propellant gas flows through the annular chamber and is heated by the heat exchanger material.