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

AKA: ROOST ISI. Status: Study 1963. Thrust: 101,842.00 kN (22,894,992 lbf). Gross mass: 6,218,000 kg (13,708,000 lb). Unfuelled mass: 435,000 kg (959,000 lb). Specific impulse: 455 s. Specific impulse sea level: 365 s. Burn time: 249 s. Height: 67.10 m (220.10 ft). Diameter: 21.30 m (69.80 ft). Span: 21.30 m (69.80 ft).

Cost $ : 154.000 million. No Engines: 18.



Country: USA. Engines: Chamber/single nozzle. Launch Vehicles: ROOST ISI. Propellants: Lox/LH2.

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