Falcon 9 - Development and Production

Development and Production

Falcon 9 v1.1
Function Orbital launch vehicle
Manufacturer SpaceX
Country of origin United States
Size
Height 69.2 m (227 ft)
Stages 2
Capacity
Payload to LEO 13,150 kg (29,000 lb)
Payload to
GTO
4,850 kg (10,700 lb)
Launch history
Status Development
First stage
Engines 9 Merlin 1D
Thrust
Burn time
Fuel LOX/RP-1
Second stage
Engines 1 Merlin Vacuum
Thrust
Burn time
Fuel LOX/RP-1

Read more about this topic:  Falcon 9

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