Definition of the term 'rocket propulsion ' per official documentation of the United States Department of Defense.
rocket propulsion
Reaction propulsion wherein both the fuel and the oxidizer, generating the hot gases expended through a nozzle, are carried as part of the rocket engine. Specifically, rocket propulsion differs from jet propulsion in that jet propulsion utilizes atmospheric air as an oxidizer, whereas rocket propulsion utilizes nitric acid or a similar compound as an oxidizer. See also jet propulsion. (US DoD)
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