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In pursuit of maximum performance, this craft was designed
with an extremely high thrust to weight ratio. Providing the
thrust is a single, afterburning, Jz/9-IPS engine. Large
twin intakes feed atmospheric reactants to a central matter
converter. This converted matter is used to fuel the
injected plasma system (IPS) reactor. In afterburning mode,
trace amounts of curium are injected into the exhaust
plasma stream to provide additional thrust.
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