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VTOHL 9t
Part of NASA SSTO 1978
American SSTO winged orbital launch vehicle. Vertical Takeoff Horizontal Landing (winged).

Status: Study 1978. Thrust: 9,222.00 kN (2,073,188 lbf). Gross mass: 687,503 kg (1,515,684 lb). Height: 70.00 m (229.00 ft). Diameter: 36.00 m (118.00 ft).

Flyaway Unit Cost 1985$: 20.000 million.

Stage Data - VTOHL 9t



Family: orbital launch vehicle, SSTO, Winged. Country: USA. Engines: SSME Plus. Launch Vehicles: VTOHL 9t. Propellants: Lox/LH2. Agency: NASA. Bibliography: 267.

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