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Falcon 9-1
LOx/Kerosene propellant rocket stage. .

Status: Retired. Thrust: 4,433.00 kN (996,578 lbf). Gross mass: 264,000 kg (582,000 lb). Unfuelled mass: 13,000 kg (28,000 lb). Specific impulse: 304 s. Specific impulse sea level: 266 s. Burn time: 180 s. Height: 29.00 m (95.00 ft). Diameter: 3.66 m (12.00 ft). Span: 4.20 m (13.70 ft).



Subtopics

Falcon 9.1-1 LOx/Kerosene propellant rocket stage. .



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