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

AKA: Vertical Takeoff Horizontal Landing. 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

  • Stage 1. 1 x VTOHL 9t. Gross Mass: 687,503 kg (1,515,684 lb). Empty Mass: 71,901 kg (158,514 lb). Thrust (vac): 11,186.092 kN (2,514,734 lbf). Isp: 467 sec. Burn time: 500 sec. Isp(sl): 385 sec. Diameter: 36.00 m (118.00 ft). Span: 36.00 m (118.00 ft). Length: 58.50 m (191.90 ft). Propellants: Lox/LH2. No Engines: 3. Engine: SSME Plus. Status: Study 1978.

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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