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Pegasus VTOVL stage
LOx/LH2 propellant rocket stage. Empty mass includes 29,600 kg of propellants used for re-entry cooling of plug nozzle and rocket soft landing at landing field.

AKA: Pegasus VTOVL. Status: Study 1966. Thrust: 23,947.00 kN (5,383,499 lbf). Gross mass: 1,250,000 kg (2,750,000 lb). Unfuelled mass: 148,000 kg (326,000 lb). Specific impulse: 459 s. Specific impulse sea level: 359 s. Burn time: 360 s. Height: 34.76 m (114.04 ft). Diameter: 10.00 m (32.00 ft). Span: 15.24 m (49.99 ft).

Cost $ : 30.000 million.



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

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