Fix docs for the afterburner attribute. AJ got stung by an ambiguity.
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@ -163,8 +163,9 @@ jet: A turbojet/fan engine. It accepts a <control> subelement to map a
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be the point of application of thrust.
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be the point of application of thrust.
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mass: The mass of the engine, in pounds.
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mass: The mass of the engine, in pounds.
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thrust: The maximum sea-level thrust, in pounds.
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thrust: The maximum sea-level thrust, in pounds.
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afterburner: Maximum additional thrust from the afterburner,
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afterburner: Maximum total thrust with afterburner/reheat,
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in pounds [0].
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in pounds [defaults to "no additional
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thrust"].
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rotate: Vector angle of the thrust in degrees about the
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rotate: Vector angle of the thrust in degrees about the
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Y axis [0].
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Y axis [0].
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n1-idle: Idling rotor speed [55].
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n1-idle: Idling rotor speed [55].
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