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SpaceX · Operational · us · Launch Vehicle

Falcon Heavy

Three-core heavy-lift variant of Falcon 9; 13 flights, all successful, most recently NASA's Roman Space Telescope in August 2026.

Verified 2026-09-24 · First flight 2018-02-06

Operator page

Systems cutaway

Systems
Falcon Heavy — systems cutaway schematicPropulsion
27× Merlin 1D+ sea-level engines across 3 cores (9 per core); RP-1/LOX; 22,819 kN liftoff thrust; center core 1× Merlin 1D Vacuum on S2.
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Structures
Three Falcon 9 Block 5 first stages strapped together; 3.7 m diameter; 5.2 m fairing.
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Recovery
Side cores land propulsively on ASDS or landing zones; center core landing varies by mission.
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Falcon Heavy70 m
Propulsion↗

27× Merlin 1D+ sea-level engines across 3 cores (9 per core); RP-1/LOX; 22,819 kN liftoff thrust; center core 1× Merlin 1D Vacuum on S2.

Structures↗

Three Falcon 9 Block 5 first stages strapped together; 3.7 m diameter; 5.2 m fairing.

Recovery↗

Side cores land propulsively on ASDS or landing zones; center core landing varies by mission.

Specs & Metrics

Payload to LEO ↑ better
63,800 kg
Maximum payload mass deliverable to low Earth orbit (~200–400 km circular), in the vehicle's stated reference configuration.
Payload to GTO ↑ better
26,700 kg
Maximum payload mass deliverable to geostationary transfer orbit (~185 × 35,786 km), in the stated reference config.
Liftoff Thrust ↑ better
22819 kN
Total first-stage thrust at liftoff (sea-level), in kilonewtons, summing all active engines and solid strap-ons.
Liftoff Mass ↓ better
1420.8 t
Total vehicle mass at liftoff including propellant, payload, and all stages, in metric tonnes.
Vehicle Height ↓ better
70 m
Full stack height at liftoff, in metres, including fairing or spacecraft.
Mission Success Rate ↑ better
100%
13 of 13 flights successful as of 2026-09-24
Percentage of launch attempts rated as full mission successes over the vehicle's complete flight history.
Launches in 2025 ↑ better
0
Total number of launch attempts conducted in calendar year 2025 (Jan 1 – Dec 31 UTC).

Subsystems

propulsion↗

27× Merlin 1D+ sea-level engines across 3 cores (9 per core); RP-1/LOX; 22,819 kN liftoff thrust; center core 1× Merlin 1D Vacuum on S2.

structures↗

Three Falcon 9 Block 5 first stages strapped together; 3.7 m diameter; 5.2 m fairing.

recovery↗

Side cores land propulsively on ASDS or landing zones; center core landing varies by mission.

Program roadmap

Falcon Heavy program roadmap2026-08-30AchievedLaunched NASA's Nancy Grace Rom…↗
  • achieved

    Launched NASA's Nancy Grace Roman Space Telescope from LC-39A; side boosters returned to the launch site

    2026-08-30↗