When you put your hand out the window of a be active car , you palpate aforce agitate against you called retarding force . This force opposes a moving vehicle , and it ’s part of the reason why your car of course slows to a full point if you take your foot off the gas foot lever . But drag does n’t just slow down auto .

Aerospace engineer are working on using the pull force out in space to develop more fuel - efficient spacecraft and missions , deorbit spacecraft without creating as muchspace rubble , and even placeprobes in area around other planets .

Space is not a complete vacuum — at least not all of it . Earth ’s atmospheregets thin with height , but it has enough tune to impart a force out of retarding force on orbit spacecraft , even up to about620 miles(1,000 kilometers ) .

NASA’s Mars Reconnaissance Orbiter used aerobraking to orbit around Mars.

NASA’s Mars Reconnaissance Orbiter used aerobraking to orbit around Mars.© JPL/NASA

As anaerospace engineering professor , I learn how drag affects the motion of space vehicle in eye socket . Aerobraking , as the name suggest , is a type of maneuver that uses the thin melodic phrase in space to utilise a drag force out in the focal point opposite to a spacecraft ’s move , much like braking in a railway car .

Changing an orbit

In space , aerobraking can change the field of a space vehicle while downplay the use of its propulsion system and fuel .   Spacecraft that area around Earth do so intwo types of orbits : circular and elliptical . In acircular orbit , the space vehicle is always at the same distance from the center of the Earth . As a upshot , it ’s always moving at the same speed . An prolate compass is stretched , so the distance from Earth− and the speed the craft moves at− changes as the ballistic capsule travels along the orbit .

The closest distributor point in an elliptical orbit around Earth , where the satellite or space vehicle is go quickest , is calledthe perigee . The farthest distributor point , where it ’s moving slowest , is calledthe apogee .

The general idea behind aerobraking is to start in a large orbitual ambit and maneuver the spacecraft into a extremely elliptical orbit , so that the lowest distributor point in the orbit− the perigree− lies in the denser part of the upper atmosphere . For Earth , that ’s between about 62 and 310 miles ( 100 and 500 km ) , with the option depending on meter required to complete the area change .

A diagram showing two orbits around circles representing planets, with the orbit labeled elliptical shaped more like an oval or stretched circle, while the orbit labeled circular is the shape of a circle.

Aerobraking brings a spacecraft from a large, circular orbit into a highly elliptical orbit, into a smaller, more circular one.

As the spacecraft passes through this lowest point , the atmosphere exerts a drag force on it , which reduces the stint of the orbit over fourth dimension . This force play rip the craft toward a circular sphere modest than the original orbit .

The first evasive action to put the spacecraft in an elliptical orbit so that drag can take gist does require using a propulsion system and some fuel . But once it ’s in the elliptical orbital cavity , drag in from the standard atmosphere slows the workmanship , and it does n’t need to use much , if any , fuel .

Aerobraking bring a craft from a large orbit to a small area and is not reversible− it ca n’t increase the size of it of an orbit . increase the size of an orbit or raising the spacecraft to a in high spirits orbit requires propulsion and fuel .

A diagram showing an oval around a dot, which represents an elliptical orbit, and two curved lines getting close to but not going all the way around the dot to represent parabolic and hyperbolic orbits.

While an elliptical orbit is closed, a hyperbolic orbit doesn’t go all the way around a planet.

Aerobraking uses

A common pillowcase where spacecraft controllers use aerobraking is when change the craft ’s orbit froma geostationary orbit− GEO− to alow Earth orbit , LEO . A GEO orbit is a circular reach with an ALT of roughly 22,236 stat mi ( 35,786 km ) . In GEO , the spacecraft crap one orbit around Earth in 24 hour , so the spacecraft always stays above the same point on Earth ’s surface .

Before aerobraking , the spacecraft ’s onboard actuation system thrusts in the opposite guidance of the GEO orbit ’s motion . This poke puts it into an egg-shaped orbit . The trade slide by through the atmosphere multiple metre , which finally circularizes the field .

Once it makes it to LEO , the space vehicle may involve to use a little bit of fuel to propel itself up into its objective orbit . Usually , the low-down breaker point of the original prolate orbit is low than the last objective rotary orbit .

The Conversation

This process is conceptually similar to how theU.S. Space Force ’s X-37B used aerobraking in early 2025 .   The U.S. Space Force describe that itsunmanned spaceplane , X-37B , used aerobraking . This psychometric test demonstrated the trade ’s agility and maneuverability .

Another software for aerobraking is to make a spacecraft deorbit− or reenter the atmosphere− after it has stopped working . This way , the caller or agency can throw away of the spacecraft and avoidcreating quad junk , since it will combust up in the lower atmosphere .

Aerobraking for interplanetary missions

A few Mars mission , including theMars reconnaissance orbiterand theMars Odyssey orbiter , have used aerobraking to get to their target eye socket around the red satellite .

For interplanetary commission like these , scientists expend aerobraking in conjunction with the craft ’s onboard propulsion system . When a spacecraft get in at Mars , it does so in ahyperbolic field .

Unlike a circular or an elliptical reach , the spacecraft ’s way of life in inflated orbit wo n’t keep it orbiting around Mars . Instead , it would wing through and depart Mars− unless it use thrust from its propulsion system to get “ fascinate ” into a closed ovate orbit .

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As the space vehicle arrives at Mars , the onboard actuation system fires to provide the force necessary to enamor the ballistic capsule into a extremely elliptical orbit around Mars . Once captured , scientists use aerobraking over several orbital passes through the atmosphere to achieve the final range , in general a circular one .

Aerobraking simulated military operation can leave in significant fuel delivery . As man get closer tolanding on the control surface of the red major planet , the fuel savings enabled by aerobraking could save mass and reserve each ballistic capsule channelise to Mars to take more supplies .

In the grand electric discharge of infinite exploration , aerobraking is not just a maneuver . It has a essential role to play in the future tense of quad operation and planetal missions and settlement .

Dummy

Piyush Mehta , Associate Professor of Space Systems , West Virginia University . This clause is republished fromThe Conversationunder a Creative Commons license . learn theoriginal article .

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