ABOUT

Heavy-lift launch vehicle composed of three Falcon 9 first-stage cores, delivering 63,800 kg to LEO with 27 Merlin engines generating over 5 million pounds of thrust

SPECIFICATIONS 11
Payload To Leo 63,800 kg
Payload To Gto 26,700 kg
Payload To Mars 16,800 kg
Stages 2
Height 70 m
Diameter 12.2 m
Thrust 22,815 kN
Propellant kerosene
Reusable Yes
Fairing Diameter 5.2 m
Liftoff Mass 1,420,788 kg
TAGS
Technology 3
Orbit & Destination 3
Application 1