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ROOST stage
Part of OOST Family
LOx/LH2 propellant rocket stage. .

AKA: ROOST. Status: Study 1963. Thrust: 165,447.00 kN (37,193,965 lbf). Gross mass: 10,898,000 kg (24,025,000 lb). Unfuelled mass: 608,000 kg (1,340,000 lb). Specific impulse: 410 s. Specific impulse sea level: 345 s. Burn time: 246 s. Height: 106.70 m (350.00 ft). Diameter: 21.30 m (69.80 ft). Span: 21.30 m (69.80 ft).

No Engines: 4.



Country: USA. Engines: 5 mlbf. Launch Vehicles: ROOST. Propellants: Lox/LH2.

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