Saturn V vs SLS

The Space Launch System is frequently described as Saturn V's successor, and the two are close in size and job description: throw a crewed spacecraft at the Moon. The differences are generational, from propellants to program cadence.

Key differences

  • Thrust and height: Saturn V stood 110.6 m with 34.5 MN of thrust; SLS Block 1 is shorter at 98 m but slightly more powerful at liftoff (about 39 MN) thanks to its solid boosters.
  • Cadence: Saturn V flew 13 times in six years at the height of Apollo; SLS has flown twice in four years.
  • Heritage: Saturn V was clean-sheet 1960s engineering; SLS reuses Space Shuttle engines, booster segments, and tooling by congressional design.
  • Payload to the Moon: Saturn V sent about 43.5 t toward the Moon; SLS Block 1 sends about 27 t, which is why Artemis splits crew and lander across two rockets.

Side-by-side specifications

Saturn VSpace Launch System
ManufacturerBoeing, North American, Douglas (for NASA)Boeing, Northrop Grumman, L3Harris (for NASA)
CountryUnited StatesUnited States
First flightNovember 9, 1967 (Apollo 4)November 16, 2022 (Artemis I)
Height110.6 m98 m (Block 1)
Diameter10.1 m8.4 m (core stage)
MassAbout 2,900,000 kg (fueled)About 2,610,000 kg
Payload to LEO140,000 kg95,000 kg (Block 1)
Stages32, plus 2 solid boosters
StatusRetired (1973)Active
Total launches13 (no failures)2 (as of July 2026)

Figures come from each article's infobox; see the articles for sources and context.

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