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Rockets and spaceflight.

A rocket the weight of a building lifts off to put a car-sized load in orbit. Why is a rocket almost all fuel, and why does it drop pieces on the way up?

Explore the scene Interactive article

01 / The experiment

Throw mass back, go forward.

Pick a propellant, change how much of the rocket is propellant, add stages, and watch the speed it has gained when the last stage burns out.

Still of the Rockets and spaceflight 3D scene, which explores: Why does reaching orbit take a rocket that is nearly all propellant?
Interactive scene

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The explanation below is available while the scene loads.

Every rocket here carries a payload of 2 % of its liftoff mass. The speed is the ideal Δv from the rocket equation. A real climb to orbit takes about eight to ten minutes; the loop shows it in a few seconds, and the stage lengths are not to scale.Gravity and air drag are left out of the speed and counted in the target instead, about 9.4 km/s for low Earth orbit, of which roughly 1.5 km/s is spent fighting them on the way up. Each stage's exhaust speed is taken as constant.

02 / Staging

Same propellant, cut differently.

Each rocket is 88 % kerosene and oxygen, 10 % tanks and engines and 2 % payload at liftoff.

Sounding rockets, boosters01

One stage

All the tanks and engines ride to the end. The last of the propellant still has to push their full weight.

Full ÷ empty, per stage
8.3
Speed at burnout
6.8 km/s
Against 9.4 km/s
2.6 km/s short
Dropped on the way
Nothing
Most launchers today02

Two stages

The first stage drops its empty tanks halfway. The second starts light, so the same propellant buys more speed.

Full ÷ empty, per stage
4.4 each
Speed at burnout
9.4 km/s
Against 9.4 km/s
Just enough
Dropped on the way
The big first stage
Moon rockets03

Three stages

Another split gains less again. Every extra stage also adds engines and separations that must work.

Full ÷ empty, per stage
2.9 each
Speed at burnout
10.2 km/s
Against 9.4 km/s
0.8 km/s spare
Dropped on the way
Two stages
The big idea

A rocket's speed grows only with the logarithm of how much heavier it is full than empty. Dropping empty stages keeps that ratio high all the way up.

Δv = ve ln(m0 / mf)

03 / The machine

Fly Apollo 11 to orbit.

Apollo 11's Saturn V, built from NASA's flight data. Drag the time from liftoff to orbit and watch the stages empty and fall away, then show one part alone, or look inside at the tanks.

Still of the machine: Apollo 11's Saturn V

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Masses, burn times, heights and speeds are Apollo 11's own, from NASA's Apollo by the Numbers (SP-2000-4029); between NASA's measured points the curves are smoothed. The rocket is drawn to its real proportions; the layout of the tanks inside each stage is approximate.

04 / The real thing

Take apart the capsule that came home.

Columbia, the Apollo 11 command module, scanned piece by piece at the Smithsonian. Take it apart, then pick a part to see where it sat inside the rest.

Still of the 3D model: Command Module Columbia, Apollo 11: forward compartment, Command Module Columbia, Apollo 11: outer shell and heat shield, Command Module Columbia, Apollo 11: cabin wall, Command Module Columbia, Apollo 11: the crew's writing on the walls, Command Module Columbia, Apollo 11: main display console, Command Module Columbia, Apollo 11: crew couches

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3D model: Smithsonian National Air and Space Museum (CC0 1.0, source)

Pushing on nothing

A rocket does not push against the ground or the air. It works best in empty space. It throws mass, its burning propellant, out of the nozzle at enormous speed, and the rest of the rocket is pushed the other way, the way a skateboarder who throws a heavy bag backward rolls forward. The faster the gas leaves, the harder each kilogram pushes. That speed, the exhaust speed, is the single most important number about a rocket engine.

To get into orbit just above the atmosphere, a spacecraft must move sideways at about 7.8 kilometres per second, fast enough that as it falls toward Earth the ground curves away beneath it. Climbing through the air and against gravity costs about another 1.5 km/s, so a launcher needs to gain about 9.4 km/s in all.

The rocket equation

Here is the catch. At liftoff, each kilogram of exhaust has to push not only the payload but all the propellant still waiting to burn. Late in the flight, with the tanks nearly empty, the same kilogram pushes far less mass and adds far more speed. Adding up all those pushes gives the rocket equation, worked out by Konstantin Tsiolkovsky in 1903:

Δv = vₑ × ln(m₀ ÷ m_f)

Δv is the speed gained, vₑ the exhaust speed, m₀ the mass full of propellant and m_f the mass once it is used up. The natural logarithm, ln, is what makes rocketry hard. Every time you double the ratio of full mass to empty mass, you gain the same fixed amount of speed, no more. To reach three times the exhaust speed, a rocket must start out twenty times heavier than it ends, which means 95 % of it must be propellant.

Why rockets come in stages

A rocket’s tanks and engines have to be big and strong enough for all the propellant at liftoff. Once most of it is burnt, that empty structure is dead weight that the rest of the propellant must keep pushing. So rockets are built as a stack of smaller rockets. When the bottom one runs dry, it falls away with its empty tanks and heavy engines, and the next one starts from a much lighter rocket.

Try it: with Exhaust speed on Kerosene, change Stages from 1 to 2 and choose On under Show the equation. The same propellant, split in two, now reaches the orbit line.

Back to the experiment

In the scene, a single kerosene rocket that is 88 % propellant reaches about 6.8 km/s, well short. Split the same propellant and structure into two stages and the speed at burnout rises to about 9.4 km/s; three stages gives about 10.2. Each added stage helps less than the one before, and each adds engines, separation hardware and things that can go wrong, which is why most launchers today use two stages, sometimes with strap-on boosters.

Faster exhaust

The other way to more speed is a better propellant. Solid-fuel motors, like big fireworks, are simple and give a huge shove, but their exhaust leaves at only about 2.5 to 2.8 km/s. Kerosene burned with liquid oxygen manages about 3.0 to 3.3 km/s. Liquid hydrogen with liquid oxygen gives about 4.4 km/s, the best of any chemical rocket in regular use. Hydrogen is so light that it needs huge, insulated tanks kept at −253 °C, which makes the structure heavier and wipes out part of the gain. In the scene, a single hydrogen stage passes the orbit line once it is about 89 % propellant. No rocket has yet reached orbit with a single stage, because real tanks, engines and losses leave too little margin.

What this model leaves out

The speed shown is the ideal speed from the rocket equation, as if the rocket were in empty space. The cost of climbing against gravity and pushing through the air is not simulated; it is added to the target instead as a rough allowance. Real exhaust speed is lower at sea level than in a vacuum, and real stages use different engines and propellants. The stages here are sized by a simple rule, each the same multiple of the mass it carries, and drawn shorter or longer than they would be so that small upper stages stay visible. The launch, the falling stages, the clouds, the rush of air and the sky darkening toward space are drawn to show the sequence, not real heights, times or distances, and the hold-down on the pad lasts longer than the few seconds a real one does.

Reuse with credit to ViewWiki and a link to this page.

06 / Learn this in a course

Practise it, step by step.

This lesson teaches the topic with checked questions.

  1. Rockets and the rocket equation Physics · Orbits and spaceflight