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Chemical propulsion: Difference between revisions

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Chemical Propulsion uses the chemical reaction between a fuel and an oxidizer to generate heat that drives the expansion of a propellant in a rocket nozzle.
Chemical propulsion uses the chemical reaction between a [[fuel]] and an [[oxidizer]] to generate heat that drives the expansion of a [[propellant]] in a rocket nozzle. The propellant is the product of the chemical reaction, for example water in the case of hydrogen and oxygen rocket engine.
 


[[Category:Propulsion]]
[[Category:Propulsion]]

Revision as of 20:41, 30 August 2021

Chemical propulsion uses the chemical reaction between a fuel and an oxidizer to generate heat that drives the expansion of a propellant in a rocket nozzle. The propellant is the product of the chemical reaction, for example water in the case of hydrogen and oxygen rocket engine.