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SpaceX · In Development · us · Launch Vehicle

Starship / Super Heavy

Fully reusable two-stage megarocket targeting 100+ t to LEO; 13 suborbital test flights, first orbital attempt (Flight 14) NET September 28, 2026.

Verified 2026-09-24 · First flight 2023-04-20

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Systems cutaway

Systems
Starship / Super Heavy — systems cutaway schematicPropulsion
33× Raptor 2/3 engines on Super Heavy booster (sea-level); 3× Raptor + 3× Raptor Vacuum on Starship upper stage; methane/LOX (methalox); 80,800 kN total liftoff thrust.
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Structures
Stainless steel 304L construction; 9 m diameter; ~71 m Super Heavy booster + ~52 m Starship upper stage; heat shield tiles on ship belly.
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Avionics
Autonomous flight termination; Starlink-derived communication backhaul; SpaceX proprietary flight computers.
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Recovery
Super Heavy booster caught by Mechazilla tower arms (first successful catch IFT-5 Oct 2024; repeated on IFT-7 Jan 2025, IFT-8 Mar 2025); Ship targets propulsive splashdown/return-to-launch-site.
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Starship / Super Heavy124 m
Propulsion↗

33× Raptor 2/3 engines on Super Heavy booster (sea-level); 3× Raptor + 3× Raptor Vacuum on Starship upper stage; methane/LOX (methalox); 80,800 kN total liftoff thrust.

Structures↗

Stainless steel 304L construction; 9 m diameter; ~71 m Super Heavy booster + ~52 m Starship upper stage; heat shield tiles on ship belly.

Avionics↗

Autonomous flight termination; Starlink-derived communication backhaul; SpaceX proprietary flight computers.

Recovery↗

Super Heavy booster caught by Mechazilla tower arms (first successful catch IFT-5 Oct 2024; repeated on IFT-7 Jan 2025, IFT-8 Mar 2025); Ship targets propulsive splashdown/return-to-launch-site.

Specs & Metrics

Payload to LEO ↑ better
100,000 kg
design target, fully reusable; up to 200,000 kg expendable
Maximum payload mass deliverable to low Earth orbit (~200–400 km circular), in the vehicle's stated reference configuration.
Liftoff Thrust ↑ better
80800 kN
Total first-stage thrust at liftoff (sea-level), in kilonewtons, summing all active engines and solid strap-ons.
Liftoff Mass ↓ better
5000 t
Total vehicle mass at liftoff including propellant, payload, and all stages, in metric tonnes.
Vehicle Height ↓ better
124 m
Full stack height at liftoff, in metres, including fairing or spacecraft.

Subsystems

propulsion↗

33× Raptor 2/3 engines on Super Heavy booster (sea-level); 3× Raptor + 3× Raptor Vacuum on Starship upper stage; methane/LOX (methalox); 80,800 kN total liftoff thrust.

structures↗

Stainless steel 304L construction; 9 m diameter; ~71 m Super Heavy booster + ~52 m Starship upper stage; heat shield tiles on ship belly.

avionics↗

Autonomous flight termination; Starlink-derived communication backhaul; SpaceX proprietary flight computers.

recovery↗

Super Heavy booster caught by Mechazilla tower arms (first successful catch IFT-5 Oct 2024; repeated on IFT-7 Jan 2025, IFT-8 Mar 2025); Ship targets propulsive splashdown/return-to-launch-site.

Program roadmap

Starship / Super Heavy program roadmap2026-03SlippedShip-to-ship propellant transfe…↗2026-05AchievedStarship V3 first flight with S…↗2026-07-24AchievedFlight 13 — 20 Starlink V3 sate…↗2026-09PlannedFlight 14 — first orbital fligh…↗2027PlannedNASA Artemis III — a Starship V…↗20262028
  • slipped

    Ship-to-ship propellant transfer flight test (NASA OIG: slipped from March 2025 to March 2026)

    2026-03↗
  • achieved

    Starship V3 first flight with Starlink simulator payload deployment (Flight 12, ~22 Starlink simulators deployed)

    2026-05↗
  • achieved

    Flight 13 — 20 Starlink V3 satellites deployed on a suborbital trajectory; ship splashed down intact, booster hit the Gulf hard

    2026-07-24↗
  • planned

    Flight 14 — first orbital flight and first Starlink V3 satellites deployed into the constellation

    2026-09↗
  • planned

    NASA Artemis III — a Starship V3 test article docks with crewed Orion in low Earth orbit; crewed lunar landings follow in 2028

    2027↗