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SASSTO stage
Part of Saturn IV
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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