why oxygen is used in satellites as oxidizer
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Rocket propellant is the reaction mass of a rocket. This reaction mass is ejected at the highest achievable velocity from a rocket engine to produce thrust. The energy required can either come from the propellants themselves, as with a chemical rocket, or from an external source, as with ion engines.
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GOX (gaseous oxygen) was used as the oxidizer for the Buran program's orbital maneuvering system.
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