name the gas filled in the rocket
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The primary performance advantage of liquid propellants is due to the oxidizer. Several practical liquid oxidizers (liquid oxygen, nitrogen tetroxide, and hydrogen peroxide) are available which have better specific impulse than the ammonium perchlorate used in most solid rockets, when paired with comparable fuels.
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Several practical liquid oxidiser ( liquid oxygen, nitrogen tetroxide, hydrogen peroxide) are available which have better specific impulse than the ammonium perchrolate used in most solid rockets , paired with comparable fuels.
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