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Falcon 9-2
LOx/Kerosene propellant rocket stage. .

Status: Retired. Thrust: 413.50 kN (92,958 lbf). Gross mass: 46,500 kg (102,500 lb). Unfuelled mass: 2,300 kg (5,000 lb). Specific impulse: 336 s. Specific impulse sea level: 0 s. Burn time: 346 s. Height: 10.00 m (32.00 ft). Diameter: 3.66 m (12.00 ft). Span: 3.66 m (12.00 ft).



Subtopics

Falcon 9.1-2 LOx/Kerosene propellant rocket stage. .



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