glappkaeft
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Chronos said:Ion rockets use extreme exhaust velocity of tiny mass particles [like ions] to achieve thrust. A conventional rocket utilizes low exhaust velocity, high mass particles [like gas molecules] to achieve thrust.
Actually you have the masses of the exhaust gasses the wrong way around. Ion engines usually use rather heavy Xenon ions (atomic weight 131). Thermal rockets however get the highest exhaust velocity by having light molecules in the exhaust. Common exhaust gases are water, CO, CO2, HF, excess H2 and similar.
For any interested parties a recommend IGNITION! An Informal History of. Liquid Rocket Propellants by John D. Clark (available at http://library.sciencemadness.org/library/books/ignition.pdf )