Saturn V liftoff thrust
Saturn V liftoff thrust is the combined force generated by the Saturn V rocket's first stage engines during launch.
How big is it?
34 MN of force
Liftoff thrust · approximate
Typical recorded range: 33 MN to 35 MN.
A little perspective
About the same scale as Space Shuttle liftoff thrust.
Space Shuttle liftoff thrust: Space Shuttle liftoff thrust is the total upward force produced by its engines and boosters to launch the shuttle from Earth.
Measurements, assumptions & sources +
Saturn V liftoff thrust
A representative 34 MN liftoff-thrust anchor for the Saturn V first stage. Engine variation and the distinction between sea-level and in-flight thrust are covered by the stated range.
Defined examples — our methodology
The marked liftoff thrust is calibrated. Unmeasured illustration details are representative.
Space Shuttle liftoff thrust
Approximately 30.5 MN at liftoff from two Solid Rocket Boosters plus three Space Shuttle Main Engines. Thrust changes through ascent and quoted totals vary with engine rating and atmospheric convention.
NASA Technical Reports Server — Space Shuttle transportation system
The marked approximate total liftoff thrust is calibrated. Unmeasured illustration details are representative.
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Why this measurement?
Why we use 34 MN
For comparison, this page uses liftoff thrust. This is labelled approximate; the central value is useful for comparison, while real values or measurement solutions can vary. The recorded range is 33 MN to 35 MN.
A representative 34 MN liftoff-thrust anchor for the Saturn V first stage. Engine variation and the distinction between sea-level and in-flight thrust are covered by the stated range.
The identifying illustration and the numerical comparison remain separate. How calibrated comparisons work →
Recorded properties
Saturn V liftoff thrust dimensions and measurements
| Property | Selected value | Recorded range | Basis |
|---|---|---|---|
| 34 MN | 33 MN to 35 MN | approximate |
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Sources and method
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