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FastTrack
Notional LOx/Kerosene rocket engine. Design concept. NASA Marshall Space Flight Center prototype experimental engine that led to Fastrac low-cost engine for X-34.

Status: Design concept. Thrust: 44.10 kN (9,914 lbf). Specific impulse: 348 s. Burn time: 325 s. Diameter: 2.00 m (6.50 ft).



Country: USA. Propellants: Lox/Kerosene. Stages: X-34A-2.

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