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Toroidal 560k
Notional LOx/LH2 rocket engine. Design concept 1990's.

Status: Design concept 1990's. Thrust: 2,491.00 kN (559,999 lbf). Specific impulse: 447 s. Specific impulse sea level: 200 s. Burn time: 204 s.



Country: USA. Propellants: Lox/LH2.

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