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How much does the biggest rocket weigh?

Short answer

The heaviest rocket ever built is SpaceX's Starship, which weighs close to 5,000 t fully fuelled on the pad; more than 90 percent of that is liquid methane and liquid oxygen. The Saturn V weighed about 2,970 t at liftoff, NASA's SLS around 2,600 t and Falcon Heavy about 1,420 t. Empty, a Starship stack weighs only a few hundred tonnes.

How much does the biggest rocket weigh?
Fourth Launch for SpaceX’s Starship (CIRA 2024-06-06)

Almost all of it is propellant

A rocket's mass on the pad says less about its structure than about its tanks. Starship, the largest vehicle SpaceX has built, weighs close to 5,000 t at liftoff, but the dry mass of the Super Heavy booster and the upper stage together is on the order of 300 t. The rest is propellant: roughly 3,400 t in the booster and 1,200 t in the ship, split between liquid methane and liquid oxygen. That ratio is typical of orbital launchers, which must carry enough energy to reach about 7.8 km/s (28,000 km/h) while fighting gravity and air drag during the first minutes of flight.

How the giants compare

The Saturn V weighed about 2,970 t (6.5 million lb) fuelled, with a first stage that alone held some 2,000 t of kerosene and oxygen. NASA's Space Launch System is lighter at roughly 2,600 t, because its solid boosters and hydrogen-fuelled core pack more energy per tonne than kerosene. The Soviet N1 came in at about 2,750 t, the Space Shuttle stack at 2,030 t and SpaceX's Falcon Heavy, the heaviest rocket in regular commercial use, at about 1,420 t. Weighing a rocket is done indirectly: engineers calculate mass from propellant loading sensors and structural measurements, since no scale under the launch mount could handle it.

Why weight sets the limits

Liftoff thrust must exceed weight by a comfortable margin. Starship's 33 Raptor engines produce about 74 MN, giving a thrust-to-weight ratio near 1.5 at ignition; Saturn V lifted off at about 1.2. That figure is why very heavy rockets accelerate slowly at first and why every extra tonne of structure costs several tonnes of propellant, which is the central trade-off in launch vehicle design.

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