Theoretical Performance of Propellants Suitable for Electrothermal Jet Engines

• 1 December 1961
• journal article
• Published by American Institute of Aeronautics and Astronautics (AIAA) in ARS Journal
• Vol. 31  (12) , 1685-1689
• https://doi.org/10.2514/8.5894

Abstract

Keywords

• THEORETICAL PERFORMANCE
• JET ENGINES
• ELECTROTHERMAL JET
• PROPELLANTS SUITABLE