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Co-axial turboramjet
Notional LH2-fuelled ramjet engine. Study 1985. Used on Sanger II launch vehicle.

Status: Study 1985. Thrust: 250.00 kN (56,200 lbf). Specific impulse: 1,200 s. Specific impulse sea level: 3,600 s. Burn time: 6,565 s.

Thrust (sl): 750.000 kN (168,600 lbf). Thrust (sl): 76,476 kgf.



Family: Ramjet. Country: Germany. Launch Vehicles: Saenger II. Propellants: Air/LH2. Stages: Sanger II-1.

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