Falcon 9

A reusable two-stage rocket optimized for satellite deployment and crew [crew] missions to low Earth orbit.

Specifications

• Height: 70 m
• Diameter: 3.7 m
• Mass: 550 t
• Payload To Leo: 22.8 t
• Propellant: RP-1/LOX
• Crew Capacity: 0
• Speed: 7.5 km/s
• Fuel Efficiency: 0.3
• Base Cost: $60M
• Landing Method: Vertical propulsive landing

Launch History

Operational since 2010, over 200 launches by 2025.