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Shuttle MDC-A-2
Part of Shuttle-2 stage series Family
LOx/LH2 propellant rocket stage. HL-10 lifting body configuration.

Status: Study 1969. Thrust: 3,070.40 kN (690,253 lbf). Gross mass: 335,601 kg (739,873 lb). Unfuelled mass: 73,442 kg (161,911 lb). Specific impulse: 459 s. Specific impulse sea level: 359 s. Burn time: 379 s. Height: 32.62 m (107.02 ft). Diameter: 7.00 m (22.90 ft). Span: 23.08 m (75.72 ft).

Cost $ : 18.000 million. No Engines: 2.



Country: USA. Engines: SSME Study. Launch Vehicles: Shuttle MDC. Propellants: Lox/LH2.

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