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Gravity and force

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 · liftoff thrust

Liftoff thrust · approximate
Typical recorded range: 38 MN to 40 MN.

Scale illustration of the liftoff thrust of an SLS Block 1, showing the recorded liftoff thrust.
Recorded liftoff thrust: 39 MN.

A little perspective

SLS Block 1 liftoff thrust vs Space Shuttle liftoff thrust: weight comparison

The liftoff thrust of an SLS Block 1 is about 1.28 times the liftoff thrust of a Space Shuttle.

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FORCE

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.

39 MNLiftoff thrust
0
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.

30.5 MNApproximate total liftoff thrust
0
Bar length measures force in newtons. Mass and local gravity determine weight.
Measurements, assumptions & sources +

SLS Block 1 liftoff thrust

Liftoff thrust: 39 MN; approximate; range 38 MN–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.

Defined examples — our methodology

The marked liftoff thrust is calibrated. Unmeasured illustration details are representative.

Space Shuttle liftoff thrust

Approximate total liftoff thrust: 30.5 MN; approximate; range 30 MN–31 MN.

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

We compare the liftoff thrust of an SLS Block 1. This is an estimate; check the notes for its rounding and uncertainty. 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 picture identifies the subject; the diagram compares the recorded values. How calibrated comparisons work →

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Recorded properties

Dimensions and measurements

PropertySelected valueRecorded rangeBasis
39 MN38 MN to 40 MNapproximate

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Sources and method

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