SLS Block 1 liftoff thrust
SLS Block 1 liftoff thrust is the total propulsive force produced by the Space Launch System Block 1 rocket at launch.
How big is it?
39 MN of force
Liftoff thrust · approximate
Typical recorded range: 38 MN to 40 MN.
A little perspective
About 1.28 times the approximate total liftoff thrust of 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 +
SLS Block 1 liftoff thrust
A representative 39 MN combined liftoff-thrust anchor for SLS Block 1. It is a rounded vehicle-level value rather than a specification for any single engine or booster.
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 39 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 38 MN to 40 MN.
A representative 39 MN combined liftoff-thrust anchor for SLS Block 1. It is a rounded vehicle-level value rather than a specification for any single engine or booster.
The identifying illustration and the numerical comparison remain separate. How calibrated comparisons work →
Recorded properties
SLS Block 1 liftoff thrust dimensions and measurements
| Property | Selected value | Recorded range | Basis |
|---|---|---|---|
| 39 MN | 38 MN to 40 MN | approximate |
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Sources and method
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