<Table> Falcon Heavy <Tr> <Td_colspan="2"> Falcon Heavy on pad LC - 39A, being prepared for its first launch </Td> </Tr> <Tr> <Th> Function </Th> <Td> Orbital heavy - lift launch vehicle </Td> </Tr> <Tr> <Th> Manufacturer </Th> <Td> SpaceX </Td> </Tr> <Tr> <Th> Country of origin </Th> <Td> United States </Td> </Tr> <Tr> <Th> Cost per launch </Th> <Td> <Ul> <Li> Reusable: $90 M </Li> <Li> Expendable: $150 M </Li> </Ul> </Td> </Tr> <Tr> <Th_colspan="2"> Size </Th> </Tr> <Tr> <Th> Height </Th> <Td> 70 m (230 ft) </Td> </Tr> <Tr> <Th> Diameter </Th> <Td> 3.66 m (12.0 ft) </Td> </Tr> <Tr> <Th> Width </Th> <Td> 12.2 m (40 ft) </Td> </Tr> <Tr> <Th> Mass </Th> <Td> 1,420,788 kg (3,132,301 lb) </Td> </Tr> <Tr> <Th> Stages </Th> <Td> 2 + </Td> </Tr> <Tr> <Th_colspan="2"> Capacity </Th> </Tr> <Tr> <Th> Payload to LEO (28.5 °) </Th> <Td> 63,800 kg (140,700 lb) </Td> </Tr> <Tr> <Th> Payload to GTO (27 °) </Th> <Td> 26,700 kg (58,900 lb) </Td> </Tr> <Tr> <Th> Payload to Mars </Th> <Td> 16,800 kg (37,000 lb) </Td> </Tr> <Tr> <Th> Payload to Pluto </Th> <Td> 3,500 kg (7,700 lb) </Td> </Tr> <Tr> <Th_colspan="2"> </Th> </Tr> <Tr> <Th_colspan="2"> Associated rockets </Th> </Tr> <Tr> <Th> Family </Th> <Td> Falcon 9 </Td> </Tr> <Tr> <Th> Comparable </Th> <Td> <Ul> <Li> Delta IV Heavy </Li> <Li> Long March 5 </Li> <Li> New Glenn </Li> <Li> Saturn C - 3 </Li> <Li> Vulcan </Li> </Ul> </Td> </Tr> <Tr> <Th_colspan="2"> Launch history </Th> </Tr> <Tr> <Th> Status </Th> <Td> Active </Td> </Tr> <Tr> <Th> Launch sites </Th> <Td> <Ul> <Li> Kennedy LC - 39A </Li> <Li> Boca Chica (under construction) </Li> </Ul> </Td> </Tr> <Tr> <Th> Total launches </Th> <Td> </Td> </Tr> <Tr> <Th> Successes </Th> <Td> </Td> </Tr> <Tr> <Th> Failures </Th> <Td> 0 </Td> </Tr> <Tr> <Th> Partial failures </Th> <Td> 0 </Td> </Tr> <Tr> <Th> Landings </Th> <Td> 2 / 3 attempts </Td> </Tr> <Tr> <Th> First flight </Th> <Td> February 6, 2018 </Td> </Tr> <Tr> <Th_colspan="2"> </Th> </Tr> <Tr> <Th_colspan="2"> Boosters </Th> </Tr> <Tr> <Th> No. boosters </Th> <Td> </Td> </Tr> <Tr> <Th> Engines </Th> <Td> 9 Merlin 1D per booster </Td> </Tr> <Tr> <Th> Thrust </Th> <Td> Sea level: 7.6 MN (1,700,000 lb) (each) Vacuum: 8.2 MN (1,800,000 lb) (each) </Td> </Tr> <Tr> <Th> Total thrust </Th> <Td> Sea level: 15.2 MN (3,400,000 lb) Vacuum: 16.4 MN (3,700,000 lb) </Td> </Tr> <Tr> <Th> Specific impulse </Th> <Td> Sea level: 282 seconds Vacuum: 311 seconds </Td> </Tr> <Tr> <Th> Burn time </Th> <Td> 154 seconds </Td> </Tr> <Tr> <Th> Fuel </Th> <Td> Subcooled LOX / Chilled RP - 1 </Td> </Tr> <Tr> <Th_colspan="2"> First stage </Th> </Tr> <Tr> <Th> Engines </Th> <Td> 9 Merlin 1D </Td> </Tr> <Tr> <Th> Thrust </Th> <Td> Sea level: 7.6 MN (1,700,000 lb) Vacuum: 8.2 MN (1,800,000 lb) </Td> </Tr> <Tr> <Th> Specific impulse </Th> <Td> Sea level: 282 seconds Vacuum: 311 seconds </Td> </Tr> <Tr> <Th> Burn time </Th> <Td> 187 seconds </Td> </Tr> <Tr> <Th> Fuel </Th> <Td> Subcooled LOX / Chilled RP - 1 </Td> </Tr> <Tr> <Th_colspan="2"> Second stage </Th> </Tr> <Tr> <Th> Engines </Th> <Td> 1 Merlin 1D Vacuum </Td> </Tr> <Tr> <Th> Thrust </Th> <Td> 934 kN (210,000 lb) </Td> </Tr> <Tr> <Th> Specific impulse </Th> <Td> 348 seconds </Td> </Tr> <Tr> <Th> Burn time </Th> <Td> 397 seconds </Td> </Tr> <Tr> <Th> Fuel </Th> <Td> LOX / RP - 1 </Td> </Tr> <Tr> <Th_colspan="2"> </Th> </Tr> </Table> <Tr> <Td_colspan="2"> Falcon Heavy on pad LC - 39A, being prepared for its first launch </Td> </Tr>

Where is the falcon heavy being launched from