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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
- 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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