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Shuttle FR-3-2
Part of Shuttle-2 stage series Family
LOx/LH2 propellant rocket stage. Trapezoidal lifting body configuration. Cross range 2419 km.

Status: Study 1969. Thrust: 4,549.05 kN (1,022,667 lbf). Gross mass: 388,189 kg (855,810 lb). Unfuelled mass: 130,159 kg (286,951 lb). Specific impulse: 459 s. Specific impulse sea level: 359 s. Burn time: 251 s. Height: 54.57 m (179.03 ft). Diameter: 7.46 m (24.47 ft). Span: 21.75 m (71.35 ft).

No Engines: 2.



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

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