Gravity and force

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.

Also known as: Space Shuttle launch thrust

How big is it?

30.5 MN of force

Approximate total liftoff thrust · approximate
Typical recorded range: 30 MN to 31 MN.

Scale illustration of Space Shuttle liftoff thrust, calibrated to its approximate total liftoff thrust measurement.
The marked approximate total liftoff thrust represents 30.5 MN.

A little perspective

About the same scale as Saturn V liftoff thrust.

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

Linear measure
FORCE30.5 MN34 MN
01
Space Shuttle liftoff thrust30.5 MNApproximate total liftoff thrust
02
Saturn V liftoff thrust34 MNLiftoff thrust
Bar length measures force in newtons. Mass and local gravity determine weight.
Measurements, assumptions & sources +

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.

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.

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Why this measurement?

Why we use 30.5 MN

For comparison, this page uses approximate total 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 30 MN to 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.

The identifying illustration and the numerical comparison remain separate. How calibrated comparisons work →

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Recorded properties

Space Shuttle liftoff thrust dimensions and measurements

PropertySelected valueRecorded rangeBasis
30.5 MN30 MN to 31 MNapproximate

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Sources and method

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