Partially reusable heavy-lift – super heavy‑lift launch vehicle
Manufacturer
SpaceX
Country of origin
United States
Cost per launch
Reusable: US$97 million (2022)[1]
Expendable: US$150 million (2017)[2]
Size
Height
70 m (230 ft)[3]
Diameter
3.66 m (12.0 ft) (each booster)
Width
12.2 m (40 ft)
Mass
1,420 t (3,130,000 lb)
Stages
2.5
Capacity
Payload to low Earth orbit
Orbital inclination
28.5°
Mass
63.8 t (141,000 lb) (theoretical)[3]
Payload to geosynchronous transfer orbit
Orbital inclination
27.0°
Mass
26.7 t (59,000 lb)[3]
Payload to Mars transfer orbit
Mass
16.8 t (37,000 lb)[3]
Payload to Pluto
Mass
3.5 t (7,700 lb)[3]
Associated rockets
Based on
Falcon 9
Comparable
Delta IV Heavy
New Glenn
Saturn C-3
Space Launch System
Vulcan Centaur
Launch history
Status
Active
Launch sites
Kennedy Space Center, LC-39A
Vandenberg, SLC-6 (future)
Total launches
9
Success(es)
9
Landings
1 center core landed (lost at sea) / 3 attempted
14 side boosters landed / 14 attempted
First flight
6 February 2018[4]
Last flight
29 December 2023
Boosters
No. boosters
2
Powered by
9x Merlin 1D per booster[3]
Maximum thrust
Sea level: 7.6 MN; 1,700,000 lbf (770 tf) (each)
Vacuum: 8.2 MN; 1,900,000 lbf (840 tf) (each)
Total thrust
Sea level: 15.2 MN; 3,400,000 lbf (1,550 tf)
Vacuum: 16.4 MN; 3,700,000 lbf (1,670 tf)
Specific impulse
Sea level: 282 s (2.77 km/s)[5]
Vacuum: 311 s (3.05 km/s)[6]
Burn time
154.3 seconds
Propellant
Subcooled LOX / Chilled RP-1[7]
First stage
Powered by
9x Merlin 1D[3]
Maximum thrust
Sea level: 7.6 MN; 1,700,000 lbf (770 tf)
Vacuum: 8.2 MN; 1,900,000 lbf (840 tf)
Specific impulse
Sea level: 282 s (2.77 km/s)
Vacuum: 311 s (3.05 km/s)
Burn time
187 seconds
Propellant
Subcooled LOX / Chilled RP-1
Second stage
Powered by
1x Merlin 1D Vacuum[3]
Maximum thrust
934 kN; 210,000 lbf (95.2 tf)
Specific impulse
348 s (3.41 km/s)
Burn time
397 seconds
Propellant
LOX / RP-1
[edit on Wikidata]
Falcon Heavy is a partially reusable super heavy-lift launch vehicle[a] that can carry cargo into Earth orbit, and beyond. It is designed, manufactured and launched by American aerospace company SpaceX.
The rocket consists of a center core on which two Falcon 9 boosters are attached, and a second stage on top of the center core.[8] Falcon Heavy has the second highest payload capacity of any currently operational launch vehicle behind NASA's Space Launch System (SLS), and the fourth-highest capacity of any rocket to reach orbit, trailing behind the SLS, Energia and the Saturn V.
SpaceX conducted Falcon Heavy's maiden launch on 6 February 2018, at 20:45 UTC.[4] As a dummy payload, the rocket carried a Tesla Roadster belonging to SpaceX founder Elon Musk, with a mannequin dubbed "Starman" in the driver's seat.[9] The second Falcon Heavy launch occurred on 11 April 2019, and all three booster rockets successfully returned to Earth.[10] The third Falcon Heavy launch successfully occurred on 25 June 2019. Since then, Falcon Heavy has been certified for the National Security Space Launch (NSSL) program.[11]
Falcon Heavy was designed to be able to carry humans into space beyond low Earth orbit, although as of February 2018[update], SpaceX does not intend to transport people on Falcon Heavy, nor pursue the human-rating certification process to transport NASA astronauts.[12] Both Falcon Heavy and Falcon 9 are expected to eventually be superseded by the Starship launch system, currently being developed.[13]
^"Capabilities & Services" (PDF). SpaceX. 2022. Archived (PDF) from the original on 22 March 2022. Retrieved 22 March 2022.
^Sheetz, Michael (12 February 2018). "Elon Musk says the new SpaceX Falcon Heavy rocket crushes its competition on cost". CNBC. Archived from the original on 3 July 2018. Retrieved 24 May 2018.
^ abcdefgh"Falcon Heavy". SpaceX. Archived from the original on 30 April 2023. Retrieved 22 April 2023.
^ abCite error: The named reference cbs-harwood was invoked but never defined (see the help page).
^"Falcon 9". SpaceX. 16 November 2012. Archived from the original on 1 May 2013. Retrieved 29 September 2013.
^Ahmad, Taseer; Ammar, Ahmed; Kamara, Ahmed; Lim, Gabriel; Magowan, Caitlin; Todorova, Blaga; Tse, Yee Cheung; White, Tom. "The Mars Society Inspiration Mars International Student Design Competition" (PDF). Mars Society. Archived (PDF) from the original on 4 March 2016. Retrieved 24 October 2015.
^Musk, Elon [@elonmusk] (18 December 2015). "-340 °F in this case. Deep cryo increases density and amplifies rocket performance. First time anyone has gone this low for O2. [RP-1 chilled] from 70 °F to 20 °F" (Tweet). Retrieved 19 December 2015 – via Twitter.
^Cite error: The named reference sxf9o20100508 was invoked but never defined (see the help page).
^"Elon Musk's huge Falcon Heavy rocket set for launch". BBC News. 6 February 2018. Archived from the original on 6 February 2018. Retrieved 6 February 2018.
^SpaceX (10 August 2018), Arabsat-6A Mission, archived from the original on 11 April 2019, retrieved 11 April 2019
^Erwin, Sandra (21 September 2019). "Air Force certified Falcon Heavy for national security launch but more work needed to meet required orbits". SpaceNews. Archived from the original on 27 April 2021. Retrieved 22 September 2019.
^Pasztor, Andy. "Elon Musk Says SpaceX's New Falcon Heavy Rocket Unlikely to Carry Astronauts". The Wall Street Journal. Archived from the original on 6 February 2018. Retrieved 6 February 2018.
^Foust, Jeff (29 September 2017). "Musk unveils revised version of giant interplanetary launch system". SpaceNews. Archived from the original on 8 October 2017. Retrieved 3 May 2018.
Cite error: There are <ref group=lower-alpha> tags or {{efn}} templates on this page, but the references will not show without a {{reflist|group=lower-alpha}} template or {{notelist}} template (see the help page).
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