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SASSTO stage
Part of Saturn IV Family
LOx/LH2 propellant rocket stage. Recoverable S-IVB with plug nozzle engine. 36 x plug-nozzle engines (102 atm chamber pressure, 6:1 mixture ratio).

AKA: SASSTO;Saturn Applications Single Stage to Orbit. Status: Study 1967. Thrust: 1,558.10 kN (350,275 lbf). Gross mass: 97,976 kg (216,000 lb). Unfuelled mass: 6,668 kg (14,700 lb). Specific impulse: 464 s. Specific impulse sea level: 367 s. Burn time: 300 s. Height: 18.80 m (61.60 ft). Diameter: 6.60 m (21.60 ft). Span: 6.60 m (21.60 ft).

Cost $ : 16.100 million. Propellant Formulation: Lox/Slush LH2.



Country: USA. Engines: Plug-Nozzle SASSTO. Launch Vehicles: SASSTO. Propellants: Lox/LH2.

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