Rocket Propulsion Systems, and Related Methods
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United States of America Patent
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Issued Date -
Aug 8, 2013
app pub date -
Jan 3, 2013
filing date -
Jan 2, 2012
priority date (Note) -
Abandoned
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Abstract
In an aspect of the invention, a system for rocket propulsion includes a heater operable to generate thermal energy from energy supplied from a non-chemical energy source, and to supply the thermal energy to a non-cryogenic fuel to thermally decompose the fuel into components that include at least a first component and a second component. The rocket propulsion system also includes a combustion chamber and a nozzle. The combustion chamber is operable to receive an oxidizer and at least a portion of the thermally decomposed fuel, and allow the two to combust. The nozzle generates thrust by directing the products of the combustion out of the system.
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