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Shuttle FR-3-1
Part of Shuttle-1 stage series Family
LOx/LH2 propellant rocket stage. Trapezoidal lifting body configuration.

Status: Study 1969. Thrust: 30,088.43 kN (6,764,148 lbf). Gross mass: 2,169,691 kg (4,783,349 lb). Unfuelled mass: 234,467 kg (516,911 lb). Specific impulse: 442 s. Specific impulse sea level: 392 s. Burn time: 275 s. Height: 71.80 m (235.50 ft). Diameter: 11.19 m (36.71 ft). Span: 25.70 m (84.30 ft).

No Engines: 15.



Country: USA. Engines: SSME Study. Launch Vehicles: Shuttle FR-3. Propellants: Lox/LH2.

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