Which has more launch thrust: Saturn V, the complete Space Shuttle stack, or SLS Block 1? NASA’s Apollo 4 account says Saturn V produced about 7.5 million pounds of thrust at Apollo 4 liftoff; NASA lists about 7.8 million pounds for the complete Space Shuttle stack; NASA lists 8.8 million pounds for SLS Block 1. These are rounded figures from the cited contexts, not a newly normalized engineering comparison. NASA’s Saturn V first-stage page gives a nearby 7.7-million-pound figure without explaining the difference, so 7.5 million is not presented as a universal Saturn V maximum.
Visuals are original illustrations, not archival NASA footage.
Sources:
- NASA — Apollo 4 Saturn V liftoff: https://www.nasa.gov/history/55-years-ago-apollo-4-the-first-flight-of-the-saturn-v/
- NASA — Saturn V first-stage page with alternate nearly 7.7M figure: https://science.nasa.gov/3d-resources/saturn-v-stage-1/
- NASA — Space Shuttle propulsion stack: https://www.nasa.gov/reference/the-space-shuttle/
- NASA — Space Launch System: https://www.nasa.gov/reference/space-launch-system/
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