EO·Atlas
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launch services

Spacex Falcon Heavy

Falcon Heavy is a three-core orbital launch vehicle that combines a central booster with two side boosters, each equivalent to a Falcon 9 first stage. Total first-stage thrust comes from 27 Merlin 1D engines (nine per core); the second stage uses a single Merlin 1D Vacuum engine. Propellants are RP-1/LOX across all stages. The vehicle shares the 5.2 m diameter fairing with Falcon 9.[1] Payload to LEO is 63,800 kg expended or 50,000 kg with all cores recovered.[1] Payload to GTO is 26,700 kg expended or 16,800 kg with side boosters recovered.[1] Side-booster recovery is routine; centre-core recovery is mission-dependent.[2] Maiden flight was 2018-02-06; first operational payload flight was 2019-04-11.[2] The vehicle is currently active.[1] EO-relevant launches include the COSMIC-2 constellation (2019, GNSS radio occultation for meteorology and ionospheric sensing) and STP-2 (2019, a DoD technology demonstration mission).[2]

Supply chain position

launched GOES-19
Sources
Cite https://eo-atlas.org/launch_services/spacex-falcon-heavy Markdown twin → Field definitions → Suggest a correction →
How to cite this page

Plain text

Spacex Falcon Heavy. EO-Atlas, SpectraWorks B.V. https://eo-atlas.org/launch_services/spacex-falcon-heavy (CC BY 4.0)

BibTeX

@misc{eoatlas:launch_services:spacex-falcon-heavy,
  title = {Spacex Falcon Heavy},
  author = {{EO-Atlas}},
  publisher = {SpectraWorks B.V.},
  note = {CC BY 4.0},
  url = {https://eo-atlas.org/launch_services/spacex-falcon-heavy}
}