# How do jetpacks work in space?

I've seen in some videos of astronauts that they used to use a jetpack type system to maneuver in the vacuum of space around the ISS and other satellites using pressurized gas.

From Wikipedia

Gaseous nitrogen was used as the propellant for the MMU. Two aluminium tanks with Kevlar wrappings contained 5.9 kilograms of nitrogen each, enough propellant for a six-hour EVA depending on the amount of maneuvering done. Typical MMU delta-v (velocity change) capability was about 80 feet per second (25 m/s).

This is perhaps a convoluted question because of the circumstances that surround my asking of this question. I was explaining to a friend that we don't really "pilot" shuttles to the moon or other objects, rather it is like a calculated throw, a one time launch that will get us to the object because of our velocity, direction, and the gravitational pull of objects in space. To that, she raised the question, "Well why do jetpacks work in space if there is nothing to push against?".

To my knowledge, there isn't anything for the gas to push against. The best answer I could muster was that expelling gas from a pressurized container still results in a force, and according to Newton's Third Law, there is an opposite force pushing the astronaut away. This can also theoretically be accomplished by throwing an object to propel yourself away from the direction of the thrown object.

I would like to know more specifically how a pressurized container creates force if there is nothing to push against, if indeed there is nothing to push against. Another question may arise from this answer, but I will save it for it's own thread.

• It works the same way a rocket works - conservation of momentum, for example. Jan 10, 2015 at 20:12
• It would be nice if you could peruse some of the articles on rocket propulsion on the Wikipedia: en.wikipedia.org/wiki/Rocket#Operation , en.wikipedia.org/wiki/Rocket_engine , and for instance, astronautix.com/engines/colodule.htm Jan 10, 2015 at 20:22
• Right, but I don't think we use rocket propulsion IN SPACE. Unless I'm wrong. This question is related specifically to how that force works in space. If it's the same and it doesn't matter whether or not there is something to push against, that's fine, just looking for that answer then. Jan 10, 2015 at 20:31
• @TomSterkenburg We certainly do - as thrusters for spacecraft, as well as in traveling to the Moon. Jan 10, 2015 at 21:09
• Do you work for the New York Times? popsci.com/military-aviation-amp-space/article/2009-07/… Jan 11, 2015 at 12:25

## 4 Answers

As you said, action = reaction, Newton's third law. In a rocket engine, a fuel is burned, creating gas that expands. Now this gas wants to expand equally in all directions. In the 'front' and 'side' directions, the gas encounters the rocket nozzle and pushes against it. In the 'rear' direction, the gas goes out the end of the nozzle and into the vacuum of space.
The gas pushing against the sides of the nozzle produces no net force: the various directions cancel each other out. But the gas pushing against the front of the nozzle has no counterpart, so there is a net force on the nozzle pointing forward.
Here's a diagram of the forces exerted by the expanding gas inside the engine:

To my knowledge, there isn't anything for the gas to push against.

That is not how a reaction engine - a family of which rockets and thrusters are a part - works.

In short: you got it backwards. The gas that is expelled is not pushing against a medium (such as the atmosphere)... the gas is pushing against the thruster. Or - to be accurate - they are pushing at each other.

The long explanation, in layperson terms: when the thruster "throws out" the gas, the work is already done. Anything that happens after the gas molecules leave the nozzle of the thruster is irrelevant. It is the process of getting the gas molecules up to speed that causes thrust.

And why is that?

Because in order to get the gas molecules up to speed, the thruster must push at them. And when that happens, the gas molecules push back at the thruster. They are both pushing the other away from them.

The long explanation, in slightly more scientific terms: when inside the fuel tank, the gas molecules are in constant motion... they are bouncing hard against the walls of the gas tank, creating pressure as they recoil back into the tank every time they impact the walls. But since the tank is closed, the net forces on the tank balance each other out.

What happens when you use the thruster is essentially that you open a hole in the side of the tank. Now there is no wall there for the gas molecules to bounce off of; instead they just escape. That means that on the other side of the tank, where gas molecules are still bouncing against the wall, there is a force that doesn't have a balancing counterpart. That means that suddenly you have a net force on the tank, and so it starts accelerating.

The short answer is "conservation of momentum" (as Bob Stein answers), but the question belies a fundamental misconception.

A propeller, helicopter rotor, or jet engine derives its thrust not from the bulk atmosphere "pushing back" but because it has accelerated some quantity of air in some direction; that air has mass, so accelerating it requires force (F = m x a). Air is a fluid; if you push on it, it just moves out of the way; there's nothing to push back - other than its own inertia. Note that propellers and helicopter rotors are just like wings; in other words, wings create lift by accelerating air downwards; there are no exceptions to this principle.

So, whether you are in an atmosphere or in the vacuum of space, what any kind of thruster is pushing against is not some bulk medium surrounding it but the propellant it is expelling - this is true for any kind of thruster (from jet packs to rocket engines).

• Great explanation. A good wing is just an efficient air-accelerator. The Wright Brothers were the first to realize that a propellor is a helically flying wing. Aug 20, 2019 at 1:20

By conservation of the center of momentum. The center of mass of a jetpack plus it's propellant stays on a constant course (along an inertial frame of reference, e.g. the ISS orbit). This remains true whether the propellant is inside or outside the jetpack. By moving a mass of propellant one way, the jet-pack-wearing astronaut moves the other way, according to this relation, the essence of rocket science:

$$m dv = -v_e dm$$

• $m$ - mass of astronaut + jetpack + remaining propellant
• $dv$ - change in astronaut's velocity
• $v_e$ - velocity of the ejected propellent, relative to jetpack
• $dm$ - mass of ejected propellent, also the change in stored propellent

By Noether's Theorem this conservation law is the same as translational symmetry, that moving through space doesn't change your laws of physics.