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Gravity and force

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 · liftoff thrust

Liftoff thrust · approximate
Typical recorded range: 33 MN to 35 MN.

Scale illustration of the liftoff thrust of a Saturn V, showing the recorded liftoff thrust.
Recorded liftoff thrust: 34 MN.

A little perspective

Saturn V liftoff thrust vs Space Shuttle liftoff thrust: weight comparison

The liftoff thrust of a Saturn V is about 1.11 times the liftoff thrust of a Space Shuttle.

Scale

FORCE

Saturn V liftoff thrust

Saturn V liftoff thrust is the combined force generated by the Saturn V rocket's first stage engines during launch.

34 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 +

Saturn V liftoff thrust

Liftoff thrust: 34 MN; approximate; range 33 MN–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.

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 34 MN

We compare the liftoff thrust of a Saturn V. This is an estimate; check the notes for its rounding and uncertainty. 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 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
34 MN33 MN to 35 MNapproximate

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Sources and method

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